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•* NBS TECHNICAL NOTE 91 " 5

U.S. DEPARTMENT OF COMMERCE/National Bureau of Standards

SELF-STUDY MANUAL

WJ

OPTICAL RADIATION

MEASUREMENTS

Part III—Applications

Chapter 1
NATIONAL INSTITUTE OF

STANDARDS & TECHNOLOGY

GAITHERSBURG, MD 20899-2500 NATIONAL BUREAU OF STANDARDS

The National Bureau of Standards' was established by an act of Congress on March 3, 1901. The Bureau's overall goal is to strengthen and advance the Nation's science and technology

and facilitate their effective application for public benefit. To this end, the Bureau conducts

research and provides: (1) a basis for the Nation's physical measurement system, (2) scientific and technological services for industry and government, (3) a technical basis for equity in trade, and (4) technical services to promote public safety. The Bureau's technical work is per- formed by the National Measurement Laboratory, the National Engineering Laboratory, and

the Institute for Computer Sciences and Technology.

THE NATIONAL MEASUREMENT LABORATORY provides the national system of

physical and chemical and materials measurement; coordinates the system with measurement

systems of other nations and furnishes essential services leading to accurate and uniform

physical and chemical measurement throughout the Nation's scientific community, industry,

and commerce; conducts materials research leading to improved methods of measurement,

standards, and data on the properties of materials needed by industry, commerce, educational

institutions, and Government; provides advisory and research services to other Government

agencies; develops, produces, and distributes Standard Reference Materials; and provides

calibration services. The Laboratory consists of the following centers:

Absolute Physical Quantities2 — Radiation Research — Chemical Physics —

Analytical Chemistry — Materials Science

THE NATIONAL ENGINEERING LABORATORY provides technology and technical ser- vices to the public and private sectors to address national needs and to solve national problems; conducts research in engineering and applied science in support of these efforts; builds and maintains competence in the necessary disciplines required to carry out this research and technical service; develops engineering data and measurement capabilities;

provides engineering measurement traceability services; develops test methods and proposes

engineering standards and code changes; develops and proposes new engineering practices;

and develops and improves mechanisms to transfer results of its research to the ultimate user. The Laboratory consists of the following centers:

Applied Mathematics — Electronics and Electrical Engineering2 — Manufacturing

Engineering — Building Technology — Fire Research — Chemical Engineering2

THE INSTITUTE FOR COMPUTER SCIENCES AND TECHNOLOGY conducts

research and provides scientific and technical services to aid Federal agencies in the selection, acquisition, application, and use of computer technology to improve effectiveness and

economy in Government operations in accordance with Public Law 89-306 (40 U.S.C. 759), relevant Executive Orders, and other directives; carries out this mission by managing the Federal Information Processing Standards Program, developing Federal ADP standards

guidelines, and managing Federal participation in ADP voluntary standardization activities; provides scientific and technological advisory services and assistance to Federal agencies; and

provides the technical foundation for computer-related policies of the Federal Government.

The Institute consists of the following centers:

Programming Science and Technology — Computer Systems Engineering.

'Headquarters and Laboratories at Gaithersburg, MD, unless otherwise noted; mailing address Washington, DC 20234. 'Some divisions within the center are located at Boulder, CO 80303.
Self-Study Manual on

mar Twi

Optical Radiation Measurements:

Part III—Applications, Chapter 1

Fred E. Nicodemus, Editor

Chapter 1. Measurement of Solar Terrestrial Spectral Irradiance in

the Ozone Cut-Off Region, Henry J. Kostkowski, Robert

D. Saunders, John F. Ward, Charles H. Popenoe, and

A.E.S. Green

Preparation and publication of this Technical Note has beei si pported by funding from

agencies listed on pp. vi & vii of the Preface.

CkAfiACat4 /\ptc>

•*»CAU 0* %

U.S. DEPARTMENT OF COMMERCE, Malcolm Baldrige, Secretary

NATIONAL BUREAU OF STANDARDS, Ernest Ambler, Director

Issued December 1982
National Bureau of Standards Technical Note 910-5

Natl. Bur. Stand. (U.S.), Tech. Note 910-5, 91 pages (Dec. 1982)

CODEN: NBTNAE

U.S. GOVERNMENT PRINTING OFFICE

WASHINGTON: 1982

For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, DC 20402

Price $5.50

(Add 25 percent for other than U.S. mailing)
PREFACE

Preparation of the NBS Self-Study Manual on Optical Radiation Measurements is an important part of our effort to meet the needs of the National Measurement System with

respect to the measurement of optical electromagnetic radiation. Significant needs exist

for measurements with uncertainties of about one percent, but the uncertainties actually

achieved are often 5 to 10 percent, or even more. These relatively poor accuracies,

as compared to those in many other types of physical measurements, result to a great

extent from the multidimensional character of optical radiation; radiant energy is distributed and may vary with position, direction, wavelength, polarization, and time.

Measurement results are also affected by various instrumental and environmental parameters.

In addition, many of those who make measurements of optical radiation have little or no training or experience in this field and are limited in the amount of time they can devote

to acquiring the needed information, understanding, and proficiency with measurement

techniques. Moreover, there are few schools that offer courses in radiometry, and there

are almost no adequate texts or references dealing with this entire subject.

The idea of producing a Self-Study Manual at NBS to try to fill some of this void was developed by one of us (HJK) in the latter part of 1973. Detailed planning got under

way in the summer of 1974 when a full-time editor (FEN) was appointed. The first nine

chapters were published in a series of four NBS Technical Notes (910- series) up to June 1979. However, subsequent progress was slowed by administrative uncertainties and

problems that affected the availability of authors (causing several changes in scheduling)

and that finally ended all direct NBS funding for the project on September 30, 1979.

Welcome transfers of funds from a number of other federal agencies were obtained to carry

the project to September 30, 1980, with the hope that it could then be restored to the NBS

budget. When that failed to materialize, outside funding was again obtained to September 30, 1981 (through FY 81).

Meanwhile, the program director (HJK) retired at the end of May 1981, and the editor

(FEN) on September 29, 1981. However, remaining FY 81 funds were used for a grant to Catholic University of America (CUA) , with whom NBS negotiated a cooperative agreement

under which CUA hired the full-time editor (FEN) who continues, as before, at NBS (same

address and telephone), working closely with the new project head (JBS) there. CUA will

also engage the services of three other former NBS employees: Dr. Kostkowski as part-time

consultant throughout the project and as author of two more chapters, and Dr. Venable and

Mr. Richmond as authors of one chapter each, as outlined in more detail below.

This Technical Note 910-5, with the first chapter of Part III—Applications, is a departure from Part I—Concepts, and the only one now scheduled. Its objectives and

significance are explained in the abstract and in the opening section, and are further

amplified below in a brief discussion of the reasons for our preoccupation with Part I

Concepts.

Our aim for the entire Manual has been to provide a comprehensive tutorial treatment

that is complete enough for self instruction. That is what is meant in the title by

"self-study"; the Manual does not contain explicitly programmed learning steps as that

term often connotes. In addition, through detailed, yet concise, chapter summaries, the

Manual is designed to serve also as a convenient reference source. Those already familiar

with a topic should turn immediately to the summary at the end of the appropriate chapter.

They can determine from that summary what, if any, of the body of the chapter they want to read for more details.

The material in the Manual is presented at the level of a college graduate in science

or engineering, but even for those with facility in college mathematics and a first course

in physics, it's not at all easy reading in spite of our best efforts at clarity and simplicity. This is an unavoidable result of the primary aim ("to make one-percent measurements commonplace") coupled with the fact that it must serve the needs of so many different

fields, including astronomy and astrophysics, mechanical heat-transfer engineering, illumination engineering, photometry, meteorology, photo-biology and photo-chemistry, optical

pyrometry, remote sensing, military infrared applications, etc.

Ill
Apparently it is very difficult for those who have not been directly involved to realize the full implications of that situation. Each of us tends to think of radiometry

and radiometric measurements in terms of our immediate experiences and requirements. What

each of us would like to have is a set of simple, carefully designed procedures, with

appropriate cautions concerning likely sources of error, for making our own particular

measurements. However, the next reader wants the same thing, but for entirely different

measurements. The desired radiometric quantities to be measured are different, the instrumentation is different, the ambient conditions are different — the possible ways in which

significant differences may exist, in terms of the radiation parameters (position, direction, spectrum, time or frequency of modulation or fluctuation, and polarization) as well

as instrumental and environmental parameters, are so numerous that any attempt to cover them all with a "cookbook" treatment of specific measurement procedures would be impossibly

unwieldy and could never be completed within any conceivable budget limitations short of

Utopia. The only way in which we can hope to effectively assist every reader who needs to make one-percent measurements is to provide you, the reader, with material which, with

sufficient effort on your part , will help you to develop sufficient understanding and

grasp of basic principles to solve your own particular measurement problems. That's why

we have concentrated on the basic material of Part I —Concepts and why it is not easy

reading. The problems of radiometry in general just aren't simple ones, even when limited

to classical radiometry in the domain of geometrical optics (ray optics) . Although we

have kept within that limitation so far, we recognize the increasingly urgent need for

similar treatment of the problems of coherent radiation and we are happy to announce that

the next chapter to be published, in a few months we hope, will be Part I, Chapter 10,

"Introduction to Coherence in Radiometry" by John B. Shumaker.

The basic approach and focal point of the treatment in this Manual is the measurement

equation, first introduced in detail but limited to the radiation parameters of position,

direction, and spectrum, in Chapter 5. We believe that every measurement problem should

be addressed with such an equation, relating the quantity desired to the data obtained,

through a detailed characterization of the instruments used and the radiation field

observed, in terms of all of the relevant parameters. These parameters always include the

radiation parameters (listed above) , as well as environmental and instrumental parameters

peculiar to each measurement configuration. The objective of the Manual is to develop the

basic concepts required so that the reader will be able to use this measurement-equation

approach. It is our belief that this is the only way that uncertainties in the measurement

of optical radiation can generally be limited to one, or at most a few, percent.

The original, overall plan for the Manual organized it into three Parts:

Part I —Concepts:

Step-by-step buildup of the measurement equation in terms of the radiation parameters,

the properties and characteristics of sources, optical paths, and receivers, and the

environmental and instrumental parameters. Useful quantities are defined and discussed,

and their relevance to various applications in many different fields (photometry, heattransfer engineering, astronomy, photo-biology, etc.) is indicated. However, discussions

of actual devices and measurement situations in this part are mainly for purposes of

illustrating concepts and basic principles.

Part II—Instrumentation:

Descriptions, properties, and other pertinent data concerning typical instruments,

devices, and components involved in common measurement situations. Included is material

dealing with sources, detectors, filters, atmospheric paths, choppers (and other types of

optical modulators), prisms, gratings, polarizers, radiometers, photometers, spectroradiometers, spectrophotometers, etc. Part III—Applications:

Measurement techniques for achieving a desired level of, or improving, the accuracy

of a measurement. Included will be a very wide variety of examples of environmental and

instrumental parameters with discussions of their effects and how to deal with them. The

examples will also be drawn from the widest possible applications in illumination engineering, radiative heat transfer, military infrared devices, remote sensing, meteorology,

astronomy and astrophysics, photo-chemistry, photo-biology, etc.

iv
That was our rather ambitious plan when we started out; limitations of support and

available resources, particularly available authors, have determined how much, or how

little, we could accomplish. So far, as indicated above, we have concentrated on Part I

Concepts. The Part I chapters already, or soon to be, published are:

1. Introduction, by F. E. Nicodemus, H. J. Kostkowski, and A. T. Hattenburg

2. Distribution of Optical Radiation with Respect to Position and

Direction—Radiance, by F. E. Nicodemus and H. J. Kostkowski

3. Spectral Distribution of Optical Radiation, by F. E. Nicodemus

and H. J. Kostkowski

4. More on the Distribution of Optical Radiation with Respect to Position and Direction, by Fred E. Nicodemus

5. An Introduction to the Measurement Equation, by Henry J. Kostkowski

and Fred E. Nicodemus

6. Distribution of Optical Radiation with Respect to Polarization,

by John B. Shumaker

7. The Relative Spectral Responsivity and Slit-Scattering Function

of a Spectroradiometer, by Henry J. Kostkowski

8. Deconvolution, by John B. Shumaker

9. Physically Defining Measurement-Beam Geometry by Using Opaque

Barriers, by Fred E. Nicodemus

10. Introduction to Coherence in Radiometry, by John B. Shumaker.

Chapters 1, 2, and 3 were in TN 910-1; 4 and 5 in TN 910-2; 6 in TN 910-3; and 7, 8, and 9 in TN 910-4. In addition, the final draft for chapter 10 (Part I) is now being revised

and should be ready for publication in TN 910-6 within one or two months following the

publication of this Technical Note 910-5.

Contingent on the availability of outside funding support, we hope that, during the

next two to three years, we can continue the current arrangements with Catholic University

of America as described above and complete the following additional chapters of Part I

Concepts:

Distribution of Optical Radiation with Respect to Time, by Fred E. Nicodemus

Linearity Considerations and Calibrations, by John B. Shumaker

Spectrophotometry, by William H. Venable, Jr. Blackbody Radiation and Temperature Scales, by Henry J. Kostkowski

Physical Photometry, by A. T. Hattenburg

Thermal Radiation Properties of Matter, by Joseph C. Richmond

Spectroradiometry of Spectral Lines, by Henry J. Kostkowski.

As stated above, the measurement-equation approach is central to the entire Manual

and the material presented in each chapter needs to be related to the approach introduced

in Chapter 5. Depending on how well this is accomplished in each chapter, there may be

need at the end to have a final summary chapter for this purpose, tying up loose ends and

putting the whole Part I into perspective. Also, examples of various categories of environmental and instrumental parameters and their significance could be usefully presented

and discussed. But it's too soon to evaluate this need at present.
Incidentally, in preparing material for the Manual, we have had the pleasure of

rediscovering the fact that the best way to learn anything is to try to teach it to someone

else. The exercise of preparing tutorial material for such wide general application has

required us to analyze our own measurement activities in a different way, broadening our understanding and resulting in improved methods and more accurate results. Note that all

references to measurement accuracy or uncertainty in this preface are concerned not only

with precision (relating to the repeatability of measurement results) but also with

accuracy (relating to agreement with the "truth" which, while unknowable in the last

analysis, is approximated by analyses and estimates based on the widest possible experience,

including agreement with measurements of the same quantities by others, particularly when

they have used different instrumentation and methods of measurement)

.

ACKNOWLEDGMENTS . The field measurements in Florida, reported in this chapter, were carried

out with the valuable assistance of the Staff of the Interdisciplinary Center for Aeronomy

and other Atmospheric Sciences (ICAAS) , Physics Department, University of Florida, and in

particular, Dr. David Doda.

We would like to thank Dr. William Fastie of Johns Hopkins University for the loan,

for testing purposes, of an early version of the spectroradiometer used in this investigation, and for various helpful discussions about this instrument.

As indicated above, we have been entirely supported by funds from other federal

agencies since September 30, 1979. This is one of the first publications since that date,

so it is our first opportunity to publicly acknowledge that most welcome support.

The project to carry out the field measurements of solar UV reported here and to analyze the data and prepare the reports, including this chapter for the Manual, has been

supported substantially by the Environmental Protection Agency, Office of Research and

Development, Washington, D.C. (Dr. Herbert L. Wiser). During the period FY 80 to the

present in FY 82, all of the other support of the Self-Study Manual Project has been from

funds provided to the National Bureau of Standards by:

DoD, CCG (tri-service Calibration Coordination Group) , Working Group for

IR/Laser (Mr. Major L. Fecteau - Army; Mr. Robert Hinebaugh - Air Force;

Dr. Felix Schweizer - Navy)

Naval Weapons Center, China Lake, California (Dr. Jon A. Wunderlich)

USAF, Air Staff, Pentagon, Washington, D.C. (Lt. Col. John E. Dunkle) through

USAF, Space Division, Los Angeles, California (Maj . Robert Chadbourne)

Naval Air Systems Command, Washington, D.C. (Mr. E. T. Hooper and

Mr. Robert C. Thyberg)

USAF, Avionics Laboratory, Wright-Patterson AFB, Ohio (Dr. Paul J. Huffman

and Mr. William J. Cannon)

Defense Advanced Research Projects Agency (DARPA) , Arlington, Virginia

(Dr. Robert W. Fossum through Dr. John Meson)

U.S. Army, BMD Advanced Technology Center, Huntsville, Alabama

(Dr. William 0. Davies)

NASA Hq. , Environmental Observation Program, Washington, D.C.

(Dr. L. C. Greenwood and Dr. S. G. Tilford)

Solar Energy Research Institute (SERI) , Golden, Colorado

(Dr. Keith Masterson)

U.S. Army, Office of Missile Electronic Warfare, Electronic Warfare Laboratory, White Sands Missile Range, New Mexico (Mr. Thomas A. Atherton)

.

VI
We are deeply indebted to a great many individuals for invaluable "feedback" tbat has

encouraged us and has helped us to put these chapters together more effectively. We renew

our strong invitation to all readers to submit comments, criticisms, and suggestions. In particular, we would welcome illustrative examples and problems from as widely different

areas of application as possible.

We are especially grateful to Mrs. Betty Castle for the skillful and conscientious

effort that produced the excellent typing and layout of still another difficult text.

Fred E. Nicodemus, Editor

John B. Shumaker, Project Head

Henry J. Kostkowski, Consultant

March 1982

Vll

Contents

Page

Part III. Applications 1

Chapter 1. Measurement of Solar Terrestrial Spectral Irradiance

in the Ozone Cut-Off Region 1

In this CHAPTER 1

THE PROBLEM — WHAT and WHY 1

MEASUREMENT CONFIGURATION 3

Approximate spectral irradiance 4

Geometry 4

Measurement with and without a diffuser 10

Calibration standard 13

MEASUREMENT EQUATION 13

OTHER FACTORS in EXPERIMENTAL DESIGN 17

Scattering and distortion 17

Wavelength accuracy 17

Computer control 19

DESCRIPTION of SPECTRORADIOMETER 19

CHARACTERIZATION of SPECTRORADIOMETER 25

Relative to magnitude 25

Relative to spectral distribution —

wavelength accuracy 26

Relative to spectral distribution —

distortion 27

Relative to spectral distribution —

scattering 28

DATA TAKING 30

Monochromator alignment 30

Alignment of standard 33

Spectral irradiance calibration ' . . . 34

Wavelength calibration 34

Solar measurements 35

IX
Page

DATA REDUCTION and UNCERTAINTIES 37

FUTURE INVESTIGATIONS 47

SUMMARY of CHAPTER 1 48

Appendix 1A Computation of Solar Terrestrial Spectral

Irradiance between 280 and 310 [nm] 52

Appendix IB Data and Results from Several Experimental Runs .... 66

References 78

Addendum to Chapter 4 in NBS Tech. Note 910-2 80
List of Figures

Page

1 Typical solar terrestrial spectral irradiance, averaged over a wavelength interval of 1 [nm] , and the action spectrum for DNA

2 Calculated solar terrestrial spectral irradiance (triangular slitscattering function with a 1 [nm] spectral slit width) 5

3 Calculated solar terrestrial spectral irradiance (0.003 [nm]

spectral slit width) 6

4 Calculated solar terrestrial spectral irradiance (0.18 and

0.34 [nm] spectral slit widths) and a 1000 [W] tungstenhalogen-standard-lamp spectrum at 50 [cm] 7

5 Set-up used for solar terrestrial spectroradiometry 8

6 Measurement configuration (without a diffuser) 9

7 Measurement configuration with a diffuser . 11

8 Angular responsivity function of NBS Solar Spectroradiometer

(without diffuser) 12

9 Relative system responsivity (without diffuser) as a function

of tracker mirror orientation (T) 15

10 Response in the cut-off region showing the effect of the long

wavelength wing of the responsivity function 18

11 Schematic diagram of dif fuser/f ilter system ..... 20

12 Detector system 21

13 Spectral transmittance of solar blind filter 23

14 Measured slit-scattering function z(X ,A) at X = 296.62 [nm]

and triangular and Gaussian functions having the same spectral width ... 29

15 Use of a laser beam to find the axes of the solar tracker 31

16 Inserts used to indicate the centers of the tracker apertures 32

17 Looking down from mirror 1 in tracker at aluminum pieces and

button used in lamp adjustment 33

18 Typical correction curve for the monochromator wavelength readout.

Maximum observed wavelength hysteresis was about 0.04 [nm] 36

19 Change with time of direct mode lamp calibrations (S' ) for 300, 335, and 345 [nm] data 45

XT
Page

A-l Simple model of earth's atmosphere showing the major constituents

that absorb or scatter solar flux in the UVB and the solar

terrestrial spectral radiance L and solar extraterrestrial

A e spectral radiance L,. q. is the vertical optical depth of

the ith constituent 54

A-2 Geometry involved in relating, through eq. (A-6) , the solar

terrestrial spectral radiance and solar terrestrial spectral

irradiance 56

A-3 Configuration for computing solar extraterrestrial spectral

irradiance E from solar extraterrestrial spectral radiance L 61

A A

List of Tables

1 Typical computer printout for a short run of data 37

2 Individual and Total Estimated Uncertainties (percent of

solar terrestrial spectral irradiance) 41

A-l Values of E? = (/. E^-z-dA) / (/. z-dA) [yW-cm~

2 -nm_1

] , eq. (A-38)

,

A AAA A A Q where E is the extraterrestrial solar spectral irradiance used

A in this chapter and z is a triangular slit-scattering function

with a width at half-height of 0.18 [nm] 64

A-2 Values of If = (/. ,E^ •z«dX)/(/. ,z«dX) [yW.cm"2 .nm_1

] , eq. (A-38),

A

J AA A ' AA

e where E is the extraterrestrial solar spectral irradiance used

A in this chapter and z is a triangular slit-scattering function

with a width at half-height of 1.0 [nm] 65

B-l Run 68 - June 18, 1980, 11:51 AM to 12 : 09 PM EST 67

B-2 Run 70 - June 18, 1980, 12:15 PM to 12:16 PM EST 68

B-3 Run 72 - June 18, 1980, 12:25 PM to 12 :28 PM EST 69

B-4 Run 60 - June 17, 1980, 12:49 PM to 12:53 PM EST 70

B-5 Run 42 (without diffuser) - June 15, 1980, 12:11 PM to 12:16 PM EST .... 72

B-6 Run 43 (with diffuser) - June 15, 1980, 12:17 PM to 12:22 PM EST 74

B-7 Run 44 (without diffuser) - June 15, 1980, 12:23 PM to 12:28 PM EST . . . . 76

Xll
SELF-STUDY MANUAL on OPTICAL RADIATION MEASUREMENTS

Part III. Applications

This is the first chapter in Part III (Applications) of

this Manual. Material developed in earlier chapters is used

to perform state-of-the-art measurements in Gainesville, Florida,

of solar terrestrial spectral irradiance between 290 [nm] and

340 [nm] . * The measurement equation is used to design the experiment and to address the effects of polarization, non-linearity,

spectral scattering, distortion, slit-scattering function, spectral irradiance calibration, and wavelength calibration. Estimates

are made of the uncertainties associated with all these factors.

The total uncertainty is estimated to be about 10 percent. An

appendix includes details for computing the solar terrestrial spectral irradiance between 280 and 310 [nm] . Suggestions are made for

reducing the uncertainty by about one third and for further research

in UV solar terrestrial measurements.

Key Words: atmospheric attenuation; atmospheric ozone; optical

radiation measurements; radiometry; solar radiation; spectroradiometry; UV spectral measurements.

Chapter 1. Measurement of Solar Terrestrial Spectral Irradiance in the Ozone

Cut-Off Region*

t by Henry J. Kostkowski , Robert D. Saunders, John F. Ward,

Charles H. Popenoe, and A.E.S. Green**

In this CHAPTER . We use the material developed in all the previous chapters of this

Self-Study Manual to illustrate how a very difficult radiometric problem is attacked and

solved. The problem is the measurement of solar terrestrial spectral irradiance between

about 290 [nm] and 340 [nm] , the region where absorption by atmospheric ozone produces a sharp cut-off in the observed spectrum. In addition to its general tutorial value, the

.chapter has applications in research on the biological effects of UV and in atmospheric

ozone determinations.

THE PROBLEM — WHAT and WHY . The optical radiation measurement problem that this chapter

addresses is the determination of the solar spectral irradiance at a point on the earth's

surface at wavelengths less than about 340 [nm] . A typical plot of the spectral irradiance (averaged over a wavelength interval of 1 [nm]) in this region is shown in figure 1, The sharp spectral cut-off is caused by absorption in atmospheric ozone.

*Equipment, experimental measurements, and analyses associated with this chapter were

extensively supported by the Environmental Protection Agency.

t Current address, Spectroradiometry Consulting, 3972 Wilcoxson Drive, Fairfax, Virginia

22031.

**Physics Department, University of Florida, Gainesville.

*Unit symbols are all enclosed in square brackets to emphasize dimensionality and encourage

routine checks of unit-dimension consistency, as discussed in Chapter 1 of Part I, on p. 8 of NBS TN 910-1.

1
280 300

- 10'

- 10

10*

320

X Cnm]

340 360

E

C

(\i

i

E

*

±

- 10'

(D

C

•H

"D

L

10_1

l

i-i

- 10-2

10

L

-P

0)

Q_

-3 CO

Figure 1. Typical solar terrestrial spectral irradiance,

averaged over a wavelength interval of 1 [nm]

,

and the action spectrum for DNA.
A major application for the measurement of solar terrestrial spectral irradiance in

the "ozone cut-off region" occurs in the many investigations that are being conducted on the effect of this radiation on living things. Optical radiation in this region is

generally damaging to animals and plants. The action spectrum (relative spectral effectiveness) for destroying DNA in cells is shown in figure 1. The damage produced by an additional increment of irradiance at 310 [nm] is a thousand times more than at 350

[nm] . Therefore accurate measurement of this solar terrestrial spectral irradiance is

important in experiments investigating its biological effect. Unfortunately, accurate

measurements of the spectral irradiance in this region are very difficult because of its

rapid change with wavelength and the very large magnitude of that change.

Another application of solar terrestrial measurements in this region is in determining

the amount of ozone in the atmosphere. This quantity is usually obtained from measurements

at wavelengths between 305 [nm] and 340 [nm] using the Dobson method [1] . Because

ozone has a much larger effect on the shorter wavelength radiation, it has been suggested

[2,3] that measurement of the shape of the solar terrestrial spectrum in the "cut-off

region" be used as a means for determining atmospheric ozone thicknesses. A major step in

pursuing this suggestion is a demonstration that the greater difficulties inherent in

these measurements do not outweigh the advantage of increased sensitivity for ozone determination.

Finally, the measurement of the solar terrestrial spectral irradiance in the ozone cut-off region is of interest to us in this Manual because it is a very difficult radiometric problem, and it provides an opportunity to illustrate the application of many of

the concepts and techniques introduced in Part I.

MEASUREMENT CONFIGURATION . The first step that should be taken in most optical radiation

measurement problems, as discussed in Chapter 5, Part I —Concepts (p. 87, 910-2) 2 [4], is

the preparation of a diagram of the entire measurement configuration. This should show

the size and location of the unknown source and the calibration standard relative to the

measuring instrument, the location of any sources of unwanted or background radiation, the

spectral distribution and approximate magnitude of the radiometric quantity of interest

for all the sources (unknown, standard, and background) , and details of the measuring

instrument including size and position of the receiving aperture, acceptance solid angle

and spectral responsivity function (Chapters 9 and 7, 910-4) [5,6].

Usually the complete measurement configuration will not be known when one begins

planning a measurement but will evolve as these plans evolve. The first bits of information will often be obtained from talking with colleagues, from technical reports, or from

Figures in brackets indicate literature references listed at the end of this chapter.

References to specific material in various chapters of the Self-Study Manual will be

given in this form — (page number or chapter, NBS Technical Note number).

3
the archival literature. In some cases, preliminary measurements must be made in order to get the required information. The final detailed configuration is only available after

the measurements have been completed. Even then, one can often use what was learned in

the first measurement to change the configuration and make a second more accurate or more

efficient measurement. We will indicate, in presenting our configuration, some of this

evolution, but, in general, the configuration described will be the one actually used in

the measurements we made in Gainesville, Florida, during June 1980.

Approximate spectral irradiance . The first thing we sought relative to the measurement

configuration was an approximation to what we were trying to measure — the spectral

distribution and magnitude of the solar terrestrial spectral irradiance. This was obtained

at a solar symposium that we had attended a few years ago and is shown in figure 1. A

report by Bener [7] and a few preliminary measurements confirmed the general shape and

magnitude shown in figure 1. The approximation was further refined by calculations 1 made

using data from the literature on extraterrestrial sunlight in high spectral resolution

and typical transmittances of atmospheric molecules, particles (aerosols) and ozone. Ultimately, a set of ozone and aerosol data obtained in our June measurements was factored

in. The distribution shown in figure 2 was calculated for a spectral slit width of

1 [nm] . It represents an average of the computed spectral irradiance weighted by a triangular slit-scattering function (p. 15, 910-4) [6] with a (full) width at half-height

of 1 [nm] . Using a much smaller spectral slit width (0.003 [nm]), the calculations of

the average spectral irradiance have the appearance shown in figure 3. Figure 4 gives the

results for spectral slit-widths of 0.18 and 0.34 [nm] with, in addition, two different

assumed conditions of atmospheric attenuation. In this latter figure we have also included

the spectral irradiance of a 1000 watt [W] tungsten halogen lamp standard at a distance

of 50 [cm].

The important points to note relative to the solar spectral irradiance distribution

are:

1. The spectral irradiance has a great deal of spectral structure

(Fraunhofer lines) so that with the spectral resolution normally

available in spectroradiometry the quantity determined will be

an average weighted by the spectral responsivity function of the

measuring instrument.

2. For a spectral slit width of 1 [nm] the averaging process

has "washed out" most of the structure.

Geometry . The next aspect of the measurement configuration we 'examined was the geometry.

The set-up available to us for making the solar measurements was in a roof-top laboratory.

A solar tracker on the roof directed the solar beam through a hole in the roof down to the

spectroradiometer, as shown in figure 5.

details of these calculations are presented in Appendix 1A.

4
10 1 E

E

C 10

*

cm

1-1

o

10"1 b

^

10"2 k-

(D

*- 1 f7"3

•H

"D

10"d -

L

L

10'4 b10"*5 bL

CL

CO

10"

10

-7

288

AX=1. 0Cnm]

292 296 300

X [nm]

304

Figure 2. Calculated solar terrestrial spectral irradiance (triangular

slit-scattering function with a 1 [nm] spectral slit width)
10' E—i—i—

r

I

*

10 1 -

^

10-

288

i r

AX = 0. 003 Enm]

J I I I I L 292 296 300

X [rim]

J I I \ I L 304

Figure 3. Calculated solar terrestrial spectral irradiance

(0.003 [nm] spectral slit width).
10

E

C 10

*

c\j

10

L

L

L

+>

0)

CL

-l

X 10"* ^-z =

(D

*- 1 f7~3

D

•H

10"* =-

10-4

10-5

10"6 k

10

-7

288 292 296 300

X [nm]

304

Figure 4. Calculated solar terrestrial spectral irradiance (0.18 and 0.34 [nm]

spectral slit widths) and a 1000 [W] tungsten-halogen-standard-lamp

spectrum at 50 [cm]. (Vertical separation of the solar curves is

due to different assumed atmospheric attenuation conditions.)
u.OO

cc

UJ

cc

IccUJ

0-< z

CO ^ t

COOLED

PHOTO-

— MULTIPLIER

CCUJo<

cc

I- t o

cc

»-zooI

I-oz

UJ

_l

UJ><

20Z0OIGC0S<l-0CC

u

<ueo

•HX)

Ct)

t-i OUUa

a)a

CO

ct) o

eno

XI

co3I u

(1) C/3

QJ

00
The tracker consists of two plane mirrors (see figure 15 as well as figure 5) . The

two mirrors can be rotated as a unit about a vertical axis through the center of the

mirror closest to the monochromator, and the mirror farthest from the monochromator can be

rotated about a horizontal axis through the centers of both mirrors. Both rotations are computer controlled [3]. The various parts of the spectroradiometer shown in the block

diagram of figure 5 will be discussed later.

Since we were interested in determining the spectral irradiance of the direct sun rather than the global irradiance (sun plus sky), we had to limit our field of view so that we included negligible sky irradiance. In order to minimize the effect of any tracking

errors, we chose a 3.25-inch [in] aperture resulting in a sufficiently large field of

view (see figure 6) relative to tracking errors but one for which we thought the sky

0.5 [DEG]

\

1.5 [DEG]

SUN

APERTURE

MONOCHROMATOR

ENTRANCE SLIT

Figure 6. Measurement configuration (without a diffuser)
irradiance would be negligible, 1.5 [deg]. Measurements made by blocking out the sun with opaque discs of various diameters confirmed that the sky irradiance was negligible 1 with the 1.5 [deg] field — about 0.5 percent that of the sun.

Measurement with and without a diffuser . Normally, spectral irradiance measurements are made with a diffuser (e.g. an averaging sphere) as the first optical element in the

spectroradiometer (p. 71, 910-2) [4], The purpose of this is to insure that the spectral

flux responsivity is invariant with direction of the incident flux. In this case, the

measurement equation (p. 65, 910-2) [4]

s ( xo

) = R •! •cos6«du)«dA«dX (1.1)

i <P A AA J AJ u

may be reduced to

s ( xo

) = R -E «dA-dX, (1.2) AA J A

which is the equation required for a measurement of spectral irradiance E. . We used a

A 1/32 [in] thick piece of teflon as a transmitting diffuser, positioning it so that it

approximately filled the field of view of the monochromator. The geometry of our measurement configuration (not to scale) using this diffuser is shown in figure 7.

There is one enormous disadvantage of the diffuser. It reduces the flux reaching the

detector by a large factor. In our case this was about 1000. Therefore, below 305

[nm] , where we were beginning to be energy limited, we rarely used a diffuser. The

entrance slit and the sun itself defined the beam geometry as shown in figure 6. In this

case, we had to rely on the flux responsivity being sufficiently uniform over the 0.5

[deg] field of view without a diffuser. It was essential to confirm that this was the case by measuring the flux responsivity as a function of angle. This was done by using a small tungsten halogen lamp providing a beam entering the monochromator with an angular

extent of 0.2 [deg] in one direction and of 0.6 [deg] perpendicular to this direction.

R (0) was obtained by determining the output signal as a function of angle of tilt of the

spectroradiometer. The result, shown in figure 8, was about the same for either orientation of the lamp. The responsivity was uniform around the peak to within 1 percent

between about -0.25 [deg] and +0.25 [deg]. This meant that the standard should be

confined to a 0.5 [deg] field of view, the angle subtended at the earth's surface by the

sun. This was accomplished by positioning the approximately 14 [mm] x 36 [mm] standard

Negligible is in reference to the overall or total uncertainty that we were striving to realize, which in these very difficult solar spectral measurements was about 5 or 10

percent.

10
APERTURE

TEFLON DIFFUSER

Figure 7. Measurement configuration with a diffuser,

lamp on the solar side of the tracker about 400 [cm] from the entrance slit of the

spectroradiometer. It was also necessary that we be able to align and maintain the

spectroradiometer orientation relative to the beam from the tracker to within 0.25 [deg]

.

For this purpose a mount was designed for the spectroradiometer which provided micrometer-

_3

type adjustments. The precision of the angular positioning was 10 ~ [rad] (0.05 [deg])

and the translational positioning 0.1 [mm].

In addition to the above described check on the uniformity of the flux responsivity, we decided to confirm by direct measurement that not using a diffuser did not greatly

degrade the accuracy. The confirmation could be made in the wavelength region between

305 [nm] and 340 [nm] where the spectroradiometer output signal was high even when the

diffuser was used. We planned to make several sets of measurements in this region with

and without the diffuser. If significant differences were found, we could then consider

using these differences to correct the shorter wavelength data where the signal was too

small to use the diffuser.

11
Figure 8. Angular responsivity function of NBS Solar

Spectroradiometer (without dif fuser)

.

12
Calibration standard . The spectral irradiance source standard usually used to calibrate

spectroradiometers in the wavelength region in which we were working (287-340 [nm]) is a 1000 [W] clear tungsten halogen lamp. Figure 4 includes a wavelength plot of the spectral

irradiance at 50 [cm] from such a standard. The spectral irradiance of this standard is

quite different from that of the sun for most of the wavelength range of interest. Also

the beam geometry (coiled-coil filament is about 5 [mm] x 25 [mm]) is different from

that of the sun. This (standard) flux also has a polarization of about 3 percent while the

sun is unpolarized. Differences between the optical radiation being measured and that of

the standard are potential sources of error [8] . In characterizing the measuring instrument, which will be discussed later, the effects of such differences will have to be

determined.

MEASUREMENT EQUATION . The general measurement equation for incoherent radiation including

polarization effects (p. 23, 910-3) [9] is

S(A

q

) =

( R

oo' L + R01* L

1 + R02* L

2 + R03*VCOse * da) ' dA' dX ' (1,3)

AX-* AA-J Aw

A similar equation is required for the standard which in our case would be located on the

solar side of the aperture shown in figure 5. This equation is

S-(A

o

) = AA AAJ Aoo s (R00' L + R01- L

l + R02* L

2

S + R 3- L

3

S)

- COSe ' d^dA - dA (1.4)

where the R_. . are the elements in the first row of a Mueller responsivity matrix repre- Oi J senting a combination of the tracker and spectroradiometer responsivities; that is (Chapter 6, 910-3) [9],

/

L

'°\

LV

L' W

R

00

R

01

R

02

R

03\ / L

R

10

R

ll

20

30 •/

responsivity

matrix

for

fresponsivity

matrix

i L_ / \ spectroradiometer/ \ tracker /

for

/ Lo\

w

(1.5)

where the L. are the components of the Stokes vector associated with the sun or the standg ard, L . Since the sun is unpolarized L.. = L„ = L„ = and

s(x

o

) = AA J AA; Ao) Rn »L «cos6 'dwdA-dA. (1.6)

Clearly, if the usual 3 percent polarized standard lamp were used, we would have to concern ourselves with a more complex measurement equation for the standard, one involving other

13
g R„ . and L.. Therefore we chose to calibrate a frosted (unpolarized) tungsten halogen

lamp by comparing it to a typical standard, using a (different) polarization- insensitive

spectroradiometer, and use this unpolarized secondary standard in our solar measurements.

s s s The measurement equation for such an unpolarized (L

1 = L„ = L„ =0) standard would

then also be

s

s (x

o

) =

'AA J AA

R_ n .Ln «cos6«da)»dA'dX. (1.7)

, s 00

Au)

Thus it appears that since both the sun and the standard lamp are unpolarized, there are no effects due to polarization. However, this is not the case. The first column of the

responsivity matrix for the tracker in eq. (1.5) is a function of the tracker orientation

[10] resulting in R„

n also changing with tracker orientation. This orientation is

determined by the time of day that the solar measurements are made. Therefore the (combined) measurement equation should be written

S(X ) ! R

on (T)«Ln -cos6«dwdA-dX

° _

•l AX J AA-l Aa) ,, QN

S

S (A ) iff RAA (T).L^-cose-dco.dA.dA

° L L L s 00 1 A\ J &AJ Aa)

and the calibration must be obtained as a function of tracker orientation, expressed here

in terms of the time (T) at which the instrument correctly points to the sun, so that

the R„

n

(T) corresponding to the time of the solar measurement is used. Figure 9 shows

how R„

n varies as a function of tracker orientation from 290 to 300 [nm] . From 300

to 340 [nm] the functional relationship is different than that at the shorter wavelengths

and also varies with wavelength.

When the diffuser is used, calibrations need not be taken as a function of tracker

orientation. In this case the spectroradiometer is unpolarized (all R. . in the spectroradiometer 's responsivity matrix, except ^nn, are equal to zero), and since the

R„

n (tracker) varies only slightly (0.1 percent) with tracker orientation [10] so does

R (spectroradiometer and tracker). In other words, although the tracker polarizes the

incoming radiation, it doesn't change the flux level significantly. Therefore when the

spectroradiometer is polarization insensitive (when using the diffuser) , the responsivity

is virtually independent of tracker orientation.

Since we wish to measure spectral irradiance, the measurement eq. (1.8) must be

modified to include E rather than L . As discussed earlier, this requires that

A A g R

nn

(T) be independent of the source solid angles Aco and Aw . Then

14
X

-p

•H

>

•H

COc

Q_

CO

0)

>

•iH -P

I—

I

0)

1.0 -

99

98

.97

.96

.95

10 11 12 13 14 15 16

Solar Tracker Orientation (T) Eh]

Figure 9. Relative system responsivity (without diffuser) as a function of tracker mirror orientation (T) . (Time

of day T is a convenient variable for designating

the orientation of a mirror that is tracking the sun.)

15
s(x

o

)

s

s (x

o

)

R

00

(T)-( L -cos6-dco)-dA-dX

AX J AA ^Ao)

AX

R

00 (T)«M LQ»cos6»daj) «dA«dX

AA V-'Acj

(1.9)

and

s(x

o

)

s

s (x

o

)

AX AA

R

oo

(T) 'VdA* dx

R

oo

(T) - E

x* dA' dx

(1.10)

AX J AA

In our application, E and E are constant over the receiving aperture area AA to well within one percent so that

s ( xo

)

s

s (x

o

)

R

00 (T).dA].dX

AX \

J AA

R

00 (T).dA).dX

AX \ J AA

(1.11)

s ( xo

) Lwt) - dX

S S (Xo

)

f E^-Rp (T).dX

Jax x e

(1.12)

-1 2 where Rp(T) [S*W «m ] is the irradiance responsivity expressed as a function of tracker

orientation, T. Under certain conditions, which will be discussed later,

S(X

q

) R^(X

o ,T).[ E

A -z(X

o ,X,T)-dX

•'ax (1.13)

S( V ^W' AXE -z(X ,X,T )-dX

X o s

where R_(X ,T) [S«W 'in ] is the irradiance responsivity factor 1 at wavelength X and

*In NBS Tech. Note 910-4 [6] (pp. 15 and 17), the responsivity factor r was defined in

terms of the relative responsivity r = z«r , and R^ = K«r = K«z«r . In this chapter

it is more appropriate to absorb K into the responsivity factor resulting in R^ = z«R^,

where R^ is called the irradiance responsivity factor . Note that R^, K, and R^

all have the same unit-dimensions [S«W «m ], while r, r , and z are dimensionless.

In general, the slit-scattering function is also a function of the polarization of the

incident flux and therefore of the tracker orientation T, as indicated in eq. (1.13).

16
tracker orientation T, and where z is the slit-scattering function (p. 15, 910-4) [6].

When the diffuser is employed, R^ or It and z will be independent of tracker orientation T.

OTHER FACTORS in EXPERIMENTAL DESIGN

Scattering and distortion . For many spectroradiometric measurements, the error produced

by assuming that E.. is constant (so that it may be moved outside of the integral sign)

A in eq. (1.12) or eq. (1.13) is not great. This is not so in our case.

The biggest problem is the unwanted response to the large and extensive (relative to wavelength) spectral flux far from the wavelength setting of the spectroradiometer that is

detected by the instrument (p. 24, 910-4) [6], This is caused by the very long wavelength

wing of the responsivity function (see figure 10) . If this wing of the responsivity

—8

function is even 10 relative to its peak, a typical value for a high-quality double

monochromator, calculations show that the amount of flux "leaked" or "scattered" at 290

[nm] for a spectral distribution similar to that in figure 1 is about equal to the actual

spectral irradiance at 290 [nm] . The amount of leakage changes very little with monochromator wavelength setting. Thus we expected significant scattering below about 293

[nm] and would probably have to determine the wings of the responsivity function experimentally and deconvolute (p. 35, 910-4) [11] the numerator of eq. (1.12) if results

accurate to 5-10 percent are desired at the short wavelengths.

In addition to the wings of the responsivity function producing an error or uncer- tainty due to scattering, the central portion can cause an error if the spectral irradiance

being measured does not vary linearly with wavelength (p. 26, 910-4) [6]. This effect is

referred to as distortion. Calculations show that the curvature 1 of the spectral distribution in figure 2 is sufficient to produce an error of about 20 percent when the spectral

slitwidth is 1 [nm] . However, if one were only interested in the average spectral irradiance over a 1 [nm] interval, the error would be reduced to about 5 percent. Because

•of the structure actually present in the spectral distribution (figures 3 and 4) , use of

a narrower spectral slit width such as 0.18 [nm] does not reduce the distortion. Therefore, deconvolution calculations (Chapter 8, 910-4) [11] of some type will be required and

for this purpose the central portion of the responsivity function will have to be determined experimentally.

Wavelength accuracy . A disadvantage of using a 1 [nm] spectral slit width as in figure

2 is that the wavelength uncertainty of the instrument would have to be limited to about

0.01 [nm] . The slope of the spectral distribution in figure 2 at 290 [nm] is about 100

percent per nanometer [nm] . The wavelength uncertainty of the best small- or mediumsized monochromators is usually 10 to 20 times larger than 0.01 [nm] . It appears that

obtaining adequate wavelength accuracy will be a problem in this measurement. One

solution would be to use a small spectral slit width and use the features of the spectral

*To see the extensive curvature one must replot the figure with a linear ordinate.

17
APPARENT i Ex

RESPONSIVITY

FUNCTION

Re

P* DUE TO

SCATTERING

WAVELENGTH X

Figure 10. Response in the cut-off region showing the effect of

the long wavelength wing of the responsivity function.

18
structure seen in figure 4 as a (wavelength) self-calibration to help reduce the wavelength uncertainty.

Computer control . Finally, careful analysis of the measurement configuration has shown

that without a diffuser — and this is the configuration required for the low spectral

fluxes below 305 [nm] — the responsivity function will depend on time (through tracker

orientation) as indicated in eq. (1.12). In addition, temporal variations in atmospheric

conditions (e.g., clouds) make it desirable to perform the measurements in as short a time as possible. On the other hand, the signal at the shortest wavelengths will be very

small and probably require integrating for 5 or 10 [min] . The flexibility required to handle these various timing problems efficiently suggests utilizing a computer for con- trolling the time sequence in which data are taken and for storing and conveniently

reducing these data.

DESCRIPTION of SPECTRORADIOMETER . After careful consideration of the various factors

discussed in the previous sections, the spectroradiometer system shown in figure 5 was designed and developed. There are four major subsystems of the spectroradiometer con- sisting of the monochromator , the detection system, the amplification and counting system,

and the computer control and data handling system.

The major monochromator specifications that were either required or highly desirable

were:

(1) Wavelength reproducibility of 0.01 [nm]

.

(2) Spectral slit width of about 0.2 [nm] and possibly 1 [nm]

.

—8

(3) A slit-scattering function that did not exceed 10

of its peak value at 50 [nm] from its peak wavelength.

(4) Angular aperture at least as large as that of an f/5 system.

(5) Spectral range at least from 280 [nm] to 370 [nm]

.

(6) Weight less than 1 [kg] and dimensions less than

25 [cm] x 25 [cm] x 50 [cm].

We were fortunate to find that Dr. William Fastie of Johns Hopkins University had

recently designed a monochromator intended to meet or exceed these specifications. A few

of these instruments had already been produced commercially. 1 We borrowed one of these

monochromators and checked its performance relative to the above specifications. All

specifications were satisfied except the wavelength reproducibility which was about five

times poorer than desired. We made some design modifications that we thought had a good

chance of improving the wavelength performance and let a contract for construction. The

major features of the final design were:

(1) All Invar 36 construction and all optical materials of Cervit

to assure thermal stability.

(2) Screw driven sine wavelength drive with stepping motor and

encoder readout to 0.001 [nm] and setability to 0.005 [nm]

.

^Research Support Instruments, Inc., 10610 Beaver Dam Road, Cockeysville, MD 21030.

19
(3) Double Ebert-Fastie (dispersion cancelling) monochromator with

focal length of approximately 125 [mm] and optical speed of f/5,

(4) Holographic gratings of 3600 [grooves per nm]

.

(5) All optical elements super polished and mirrors coated in

such a way as to optimize high specular reflectance and

low diffuse reflectance (scattering).

(6) Fixed (non- adjustable) slits with spectral slit widths

of 0.2 [nm] and 1 [nm]

.

(7) Weight less than 4.5 [kg] and dimensions less than

15 [cm] x 15 [cm] x 30 [cm].

The cost was approximately $27,000 in 1980.

RETAINING RING

& ENTRANCE APERTURE

WHEN DIFFUSER IS USED

DIFFUSER OR FILTER

OPTIC AXIS

FIRST GRATING

MONOCHROMATOR

ENTRANCE SLIT

COLLIMATING MIRROR

Figure 11. Schematic diagram of dif fuser/f ilter system.

20
The above monochromator did not include a means for mounting diffusers or filters in

front of the entrance slit or a cooled detector following the exit slit. These additions were designed and fabricated at NBS.

The dif fuser/f ilter mounting system allowed for rapid, reproducible placement or interchange of filters and provided a means of easily locating the optic axis of the

instrument for alignment purposes. Figure 11 is a schematic diagram of the system. The

tube, shown in the figure, is mounted by screws onto the front (entrance-slit portion) of

the monochromator in a position so that it is coaxial with the monochromator 's optic

axis. 1 The cap, when screwed tightly on the tube, conveniently insures good reproducibility in positioning filters. One normally would have as many caps as filters or combinations of filters.

A schematic diagram of the detection system is shown in figure 12. The quartz lens

and photomultiplier are positioned so that the exit slit is defocused on the cathode of

the photomultiplier. The larger area of irradiation minimizes the effects (noise and

instability) of cathode non-uniformity and of small vibrations or motions.

QUARTZ LENS THERMOELECTRIC COOLER

MAGNETS

QUARTZ WINDOWS

Figure 12. Detector system.

^he optic axis is the central ray of the full optical beam that can traverse the monochromator. Normally for a well-aligned monochromator, the optic axis passes through the

centers of all the slits and the centers of all the optical elements. A small HeNe laser

is useful for establishing the optic axis and the alignment of this axis relative to the

tracker or external apertures.

21
The purpose of the ring magnets is to reduce the effective size of the cathode. The

magnetic field produced by the rings permits only those thermal electrons that are emitted

from about a 0.5 [in] diameter area of the cathode to strike the first dynode. This

factor plus cooling to about -20°C with the thermoelectric cooler minimizes dark current

(or dark counts) which is particularly important at the low flux levels at wavelengths

below about 292 [nm]

.

The photomultiplier has a bialkali cathode and was selected for high quantum efficiency and low dark count. In order to reduce the amount of scattered signal detected, a Cs-Te (solar blind) cathode was considered. However, a bialkali cathode together with a "solar blind" filter (transmittance shown in figure 13) accomplishes the same thing but

with a higher quantum efficiency at 290 [nm]

.

The output signal of a photomultiplier, resulting from an incident photon that has

ejected a photo-electron, consists of a burst or pulse of electrons lasting only a few

nanoseconds. When the photon rate (incident flux level) is high these occur too close

together (may even be superimposed) for them to be detected individually. The average

electron flow must be measured. This is the so-called current measuring mode which is

used in most radiometric applications using photomultipliers. However, when the flux

level is low, as in our case at the shorter wavelengths, these electron bursts or pulses

are sufficiently separated so that they can be detected individually. This is the photon

counting mode. Because the flux level at wavelengths below 295 [nm] is so low, we decided to use the photomultiplier in a photon counting rather than a current measuring

mode.

The photon counting mode has a number of advantages over the current measuring mode.

Noise and dark counts (signal counts when a shutter is in place so that the flux being

measured is blocked or shuttered) can usually be reduced, relative to the current mode,

because most pulses that are produced by sources other than incident photons (e.g.

thermionic electrons and stray electrons from dynodes) have a smaller amplitude and can

be rejected by proper setting of the threshold voltage in the discriminator (see figure

5). Noise from electronic components and connections, leakage currents, power lines, and

external fields can be made insignificant or minimized through digital processing and

counting procedures. The average signal in the current measuring mode is directly affected

by all the above types of noise but the number of pulses per second in the photon counting

mode is not. Another advantage in the photon counting mode is that the counting rate is

not as highly sensitive to the dynode voltages as is the average signal in the current

measuring mode. Thus, much less stability and control are required in the high voltage

power supply used for supplying the dynode voltages.

One disadvantage of the photon counting mode is that, for very high photon fluxes,

the observed counting rate S' [cs ] is not exactly proportional to the incident flux.

This is because there is a significant probability of two photons arriving within the

resolving time (dead time) of the instrument (pulse overlapping) . Without this

22
10

(D

c

+>

-p

•H

E

CO

c

L

10-l

10"2

10-3

280 300 320

X [nm]

340 360

Figure 13. Spectral transmittance of solar blind filter,

23
proportionality (linearity), we can't do many of the things with the measurement equation

that we would like to do. 1

Fortunately there is an easy way of handling the non-linearity in the current problem.

This is done by assuming that the flux responsivity is constant (linearity exists) and

then correcting the observed output signal to what it would have been if this constancy

had actually existed. Operationally one might think of the "detector" as consisting of

the photomultiplier and associated electronics together with a computer or hand calculator

which provides a correction from the indicated deficient rate S' to a quantity S that

is exactly proportional to the actual incident photon flux. An approximate relationship

between S' and S is [12]

S/S' = C(S') = 1 + t-S' (1.14)

where C(S') is the "correction factor" for transforming the observed counting rate

S' [c«s ] to the "correct" counting rate S, and t [s*c ] is the resolving time of

the system. Differences between S' and S can be quite significant. For example, with

— 7 —1 ft — 1 t = 10 [s«c ], a typical value, and S' = 10 [cs ], the "correct" counting rate

differs from the observed counting rate by 10 percent.

High quality photon counting systems are now available commercially as "shelf items."

We selected one of these for this application. The major points to consider in this

selection are over-all stability and ease of operation and required resolving time and

integration time.

The computer control and data handling system is the remaining subsystem (figure 5)

to be discussed. This subsystem consists of a 48K RAM microcomputer, dual floppy

8 [in] disk drive, terminal/video screen and printer. We purchased standard, readily

available commercial items. The electronic circuitry (interfacing) required to couple

the computer system to the rest of the spectroradiometer was designed and constructed at NBS. This is not a difficult task for a digital electronic engineer. It is also possible

to obtain the interface electronics commercially.

The computer can be programmed to start measurements at a particular wavelength,

integrate the counts for any time interval from a fraction of a second to hours and

repeat this at any other wavelength or group of wavelengths. In addition to the

*When the measurement equation was first derived in Chapter 5 [4], we indicated that the

assumed constancy of the flux responsivity with respect to the magnitude of the flux was a convenience. However, we have come to realize that it is a necessary assumption for much

that we want to do when applying the measurement equation. Examples of this are in going

from eq. (1.12) to eq. (1.13) and in the definition R = K>z-r . (See footnote on page

16.) An in-depth treatment of linearity is planned for a forthcoming chapter of this

Manual

.

24
wavelength, total signal counts, and counts per second, the ambient temperature, time,

and date are also recorded. As data are obtained they may be viewed on the video screen,

and/or printed and stored on a floppy disk. Printing the data is usually delayed until

all observations for the day are complete because concurrent printing increases the time

required to perform the experiment.

CHARACTERIZATION of SPECTRORADIOMETER . In order to minimize the errors or uncertainties

of a radiometric measurement-, the measuring instrument's responsivity should be determined

as a function of each radiation parameter for which there are significant differences

between the unknown radiant flux being measured and that of the standard. The pertinent

radiation parameters were discussed in the sections on the measurement configuration and

the measurement equation. The two radiation fluxes in this problem were the sun and a frosted 1000 [W] tungsten halogen lamp at 400 [cm]; the parameters for which the two

fields differed significantly were magnitude (absolute value of the spectral irradiance)

and spectral distribution.

Relative to magnitude . As pointed out earlier, the responsivity of photomultipliers

when used as photon counters decreases at sufficiently high levels of incident photon

flux in accordance with eq. (1.14). With the very large magnitude and variation of

magnitude of the solar terrestrial irradiance in the spectral region of interest, these

decreases (non-linearity) could be significant. This problem has been addressed by

determining C(S') of eq. (1.14) and using the "corrected" output signal S = C(S')«S'

instead of the observed signal S' in the measurement equation. In this way linearity

with all its desirable features is effectively maintained.

The correction C(S') was obtained by first determining the spectral transmittance

t of a filter at a sufficiently low incident flux cj> . (and corresponding low observed

counting rate S') where C(S') = 1 and then repeating the measurement of t with

higher incident flux levels up to the highest flux level or counting rate obtained in the

solar measurements. 1 In order to achieve a more accurate approximation, the power series

in S' [eq. (1.14)] was carried to one more term; i.e.,

C(S') = S/S' = 1 + t-S' + u-S'

2

. (1.15a)

^-This technique can be used in the current problem because it is well established that

for photomultipliers, when the counting rate is sufficiently low, S' = R-$ and therefore

$ S

t n

t = — = -r-f-. Otherwise, if the responsivity of a detector were such that S' = R«$ at

i i

low levels, S'/S'. would still be constant as a function of S! at sufficiently low

- t i i

q » „

i but equal to x instead of x. These filter measurements alone will not determine

the value of the exponent n.

25
The transmittance t of the filter referred to above would then be

t = C'(SJ) • S^/[c(Sp • Sj] (1.16a)

For S' sufficiently small C(S!) = C(S') = 1 and t = S'/S^. For larger values of S|,

substituting eq. (1.15a) into eq. (1.16a)

t = (s'

t + fS' 2 + u-S^3)/(s^ + t-S^

2 + u-S^3

) (1.16b)

and rearranging terms

tS^ - Sj. = (S^

2 - T-S^

2).t + (S^

3 - x-S^3 )-u. (1.16c)

Measurements of t, S! and S' were performed with the 253.7 [nm] spectral line

from a temperature-stabilized low-pressure mercury-discharge lamp source from which the

irradiance (flux) level was varied by the insertion of additional filters, taking care not to disturb the geometry of the beam incident on either the filter being measured or on the monochromator. Using these data, t and u were obtained from a least squares

fit of eq. (1.16c). For values of S' as high as 2.5*10 [c«s~ ],

S/S' = C(S') = 1 + 6.927«10~8

«S' + 7.174-10

_15

-S'

2 (1.15b)

where S is the "corrected" output signal and S' is the actually observed output

signal in [cs ].

There was another problem relative to the responsivity that we uncovered which is

significant at very low counting rates. In our system, about once every 5 [min] , we witnessed a burst of 50 to 100 counts. This means about a 1 percent error for a counting rate of 30 [cs ] when integrating for 5 [min] and larger errors at lower

counting rates. This effect was not significant down to 290 [nm] because the lowest

counting rate at this and longer wavelengths was about 40 [cs ]. The effect was significant at shorter wavelengths because the lowest counting rate was about 5 [cs ] at 289 [nm] , 2 at 288, and 1 at 287. However, we did not try to solve this problem

because scattering was a serious problem below 290 [nm] , and, as you will see shortly, we were not able to correct for this scattering. So an additional error was immaterial.

We were only able to satisfy our desired overall 5-10 percent uncertainty at wavelengths of 290 [nm] and higher.

Relative to spectral distribution — wavelength accuracy . The most obvious concern relative to the large difference in spectral distribution between the standard source and

the sun is that of wavelength accuracy. The spectral irradiance of the sun falls off at

26
a rate of about 1 percent per 0.01 [nm] . Therefore a wavelength uncertainty of 0.01 [nm] or less is desired.

The first step in characterizing the spectroradiometer relative to wavelength was to check its reproducibility. The 296.728 [nm] mercury spectral line from a low pressure

mercury source was used for this purpose. With the spectral slit width of the instrument

being 0.2 [nm] , the "peak" of the line was too broad to utilize its position to check

wavelength reproducibility to 0.01 [nm] . A wavelength reference which is orders of magnitude more sensitive than the peak of a spectral line is the steep sides of the line.

When the spectral slit width is large compared to the spectral line width, this is really

the side of the slit-scattering function. A suitable region to use is that part of the

_2 spectrally scanned line which is a factor of 10 less than the peak. The rate of change

_2

of signal with wavelength at 10 of the peak is at least 50 percent per 0.01 [nm]

compared to about 0.5 percent per 0.01 [nm] at the peak.

We found that the wavelength reproducibility for our monochromator varied from 0.01

[nm] to about 0.05 [nm] depending on the prior (immediate) history of the wavelength

drive and setting. The 0.01 [nm] figure relates to scanning repeatedly over a spectral

line, covering a range of about 1 [nm] and taking a few minutes for each scan. The 0.05

[nm] reproducibility corresponds to scanning repeatedly over the line but covering a range

of about 60 [nm] or 30 [min] for each scan. By cleaning, tightening, adjusting, and

lubricating, it was possible to improve the 0.05 [nm] only slightly to 0.04 [nm] . It was clear that to achieve 0.01 [nm] wavelength uncertainty would require a data-taking

schedule (short-term, small wavelength range repetitive scans) that was not practical in

most cases. Another possiblity for realizing a 0.01 [nm] reproducibility was to use the

solar structure shown in figure 4 to perform a wavelength self-calibration in each experimental run.

In addition to the short-term reproducibility just discussed, wavelength accuracy may

also depend on somewhat longer term changes (few hours) caused by ambient temperature

variations. The effect of instrument temperature on wavelength setting was checked and

found to be only about 0.01 [nm] per 3 [°C] change in temperature. This was considered

to be an insignificant factor in our case compared to the short-term reproducibility.

Wavelength accuracy is also affected by any lack of symmetry in the slit-scattering

function, particularly when the wavelength determination is made by the technique (sides of

slit-scattering function) described earlier. This will be discussed in the next section

along with the effects of distortion and scattering.

Relative to spectral distribution — distortion . The central portion of the slit-scattering function is required in order to ascertain and correct for the amount of distortion.

-2

We determined the central portion of the slit-scattering function down to about 10 of

its peak value by spectrally scanning over various mercury lines between 289.4 and 365

_2

[nm] . It was not possible to get lower than about 10 with a mercury line because of

27
the background radiation from other lines, particularly the 254 [nm] line. For values

-2

below 10 , we used a laser line at 290 [nm] . We obtained this UV line from a tunable

CW dye laser operating at 580 [nm] by frequency doubling with an appropriate crystal.

The laser beam was positioned along the optic axis of the monochromator with the diffuser

in place. The size of the beam was adjusted so that the instrument was irradiated with

about the same solid angle as that subtended by the sun. A spectral scan over these lines

should be a good approximation to the central portion of the slit-scattering function (p.

20, 910-4) [6]. When irradiated on axis, the central portion was quite asymmetric. However, the degree of asymmetry changed with the direction of the beam entering the monochromator. It was possible to find a particular direction slightly off axis, for which

good symmetry was realized. This was done and all solar measurements made without the

diffuser were made with the solar beam incident from this direction. The asymmetry was also quite pronounced in the diffuse mode; that is, with the diffuser filled with optical

radiation. However, by trial and error, it was possible to find an area on the diffuser

(equal to about one-half the total area) which also resulted in a symmetric slit-scattering

function.

Figure 14 shows an example at 296 [nm] of that portion of the slit-scattering function obtained with the mercury lines. Also shown are triangular and Gaussian functions

having the same spectral slit width. These functions do a fair job of representing our measured slit-scattering function down to about 0.3 of its value. From 0.3 to about

10 , a much better representation is the following function:

z(A ,A) = exp[-126.38-(A -A)

2

] +h exp[-2. 983-10 3 -(A -A)

2

-1.2037-104 -(A

o-A)

4

],

(1.17)

where A is the monochromator setting and A is the wavelength in nanometers [nm] . The

° -5

slit-scattering function for values less than 10 " is discussed in the next section.

Incidentally, the spectral slit width varied slightly with wavelength from 0.183 [nm] at 289 [nm] to 0.165 [nm] at 312 [nm] and then back to 0.176 [nm] at 334 and 365 [nm]

.

Convolution calculations indicated that it was more important, relative to distortion

effects, to know that the slit-scattering function was symmetric than to know its exact

shape or width. Also, the existence of symmetry meant that wavelength calibrations could

be performed by determining the average of the wavelengths on the two sides of the slit-

-2

scattering function where the value of the function is about 10 of its peak value.

Relative to spectral distribution — scattering . In order to correct for scattered radiation that we anticipate to be significant below about 292 [nm] , the long wavelength wing

of the slit-scattering function is required. We tried to obtain these wings with our tuned

UV laser, but the signal-to-noise ratio was too small to get lower than about 2 x 10 ,

28
1

i

/

\

i i

Measured

('

1

\\ Trianqular

. 9

1

1

I

1

\

\\ - Gaussian

. 8

V

/-N X " ?' \

JV

1

V

TM\-6

1

II

1 \\

CD 1

ll

\\

a «3 .5

CD \

CM

^^ /f . 4

N iin n \

. 3

if

i

1

\\ . \1

. 2

!'\

s —

. 1

r"

ft

ij

r i , V,

—

-.2 -.1

X

- X [nm]

. 1 . 2

Figure 14. Measured slit-scattering function z(A ,X) at X 296.62 [nm]

and triangular and Gaussian functions having the same spectral width.

29
even with an integrating time of one hour. The 2 x 10 was the value at about 1.8

[nm] from the peak. We obtained a rough idea of the magnitude of the more distant wing

by scanning over the short wavelength portion (p. 22, 910-4) [6] of the 253.7 [nm]

spectral line from a very intense low pressure mercury source using suitable filters to remove radiation other than that scattered from the 253.7 [nm] line itself. At 200

—8

[nm] the result was 1.4 x 10 . Thus the slit-scattering function at +53.7 [nm]

—8

(i.e., 253.7-200) from the peak is about 10 when the monochromator is irradiated

with highly incoherent radiation that fills the f/5 field of view.

So, much to our disappointment, we were not able to obtain an accurate (5 or 10

percent) determination of the distant wing of the slit-scattering function and would

not be able to accurately correct for Scattering. This will be possible when a tunable

laser is available with about 10 [mW] of power at 290 [nm] . Until then, the short

wavelength limit for our accurate measurements will be determined by the wavelength at which scattering begins to be significant. The solar data itself will reveal this

wavelength, as will be shown shortly.

DATA TAKING . In this section we discuss not only details of the actual data taking but

also alignment of the monochromator relative to the sun, alignment of the tungsten lamp

standard, and calibration using the standard.

Monochromator alignment . Careful alignment of the monochromator was essential prior to making any solar measurements, particularly when the diffuser was not used. Figure 8 shows that an angular misalignment of a degree would result in a significant error. Also, as mentioned in the previous section, an angular misalignment would destroy the

spectral symmetry of the slit-scattering function., reducing wavelength accuracy and

increasing distortion.

The monochromator was aligned in the following manner. A low-power He/Ne laser was

set up in the laboratory and aligned so that its beam passed upward approximately through

the center of the solar tracker. Then the laser was fine-adjusted in position and

orientation so that its beam (see figure 15) did not move relative to the upper aperture

when the tracker followed the sun. This meant that the laser beam was striking each

tracker mirror at the intersection of the plane of the mirror with the vertical and

horizontal axes of rotation, as indicated in figure 15. After this condition was

realized, the upper aperture was positioned and secured so that the laser beam passed

through its center. The 5 [in] diameter lower aperture was also positioned so that

the laser beam passed through its center. Next the laser was set up on the roof and

again aligned so that its beam went downward through the centers of both apertures. The

monochromator was then positioned and oriented so that the laser beam struck the center

of the entrance slit and coincided with the optic axis. This was easy to accomplish

because the tube of the dif fuser/f ilter system had been made and mounted so that its top

surface was perpendicular to the optic axis. A microscope cover glass placed on this

surface was therefore perpendicular to the optic axis and the monochromator was rotated

30
VERTICAL AXIS

OF ROTATION

MIRROR 1 ROOF

X

LABORATORY

3.25 [In]

UPPER

APERTURE

HORIZONTAL AXIS

OF ROTATION

MIRROR 2

S

5 [In] LOWER APERTURE

LASER BEAM

Figure 15. Use of a laser beam to find the axes of the solar tracker.

31
until the laser beam retroref lected back on itself (or the center of the 5 [in]

aperture). Finally, the monochromator was rotated about its entrance slit by the amount

required (0.4 [deg]) for a spectrally symmetric slit-scattering function.

In performing the above alignments it was essential to use a heavy, stable, laser

mount with micrometer adjustments for translation and two orthogonal rotations about axes perpendicular to the laser beam. In addition, it was convenient to use circular

aluminum inserts each with a translucent "button" with a small hole drilled through the

center as shown in figure 16. The insert could be placed in the aperture and used as a convenient indicator of the aperture center while adjusting the laser beam.

CIRCULAR ALUMINUM INSERT

TRANSLUCENT BUTTON

WITH CENTER HOLE

W///////////M Wmzmzzzzp

uuunuuuuus szzznznzmzzm

APERTURE

Figure 16. Inserts used to indicate the centers of the tracker apertures.

32
Alignment of standard . For the spectroradiometer calibration it was necessary to position the standard lamp precisely. The procedure was as follows. The He/Ne laser was mounted on the roof above the tracker and aligned until the laser beam went through the

center of the button in the upper aperture insert (see figure 16) and was incident on the

center of the monochromator entrance slit. Another insert similar to that in figure 16 was fitted into a rectangular piece of aluminum and positioned in the lower aperture as indicated in figure 17 so that the laser beam traversed its button also. The laser was then set up in the laboratory and aligned so that its beam traversed the buttons in the

lower and upper apertures in the opposite direction. Then, the tungsten standard was mounted on the roof tracker so that its center was irradiated by the laser beam. The lamp

mount was an aluminum tubular structure of sufficient lightness pot to limit the smooth

motions of the tracker and of sufficient rigidity so that the lamp was stably positioned

relative to the 3.25 [in] tracker aperture. The distance between the entrance slit and

the lamp was selected, as mentioned earlier, so that the lamp's largest dimension subtended about 0.5 [deg] (same as the sun) at the entrance slit. The actual distance was measured to be 396.3 [cm] with an uncertainty of about 0.5 [cm].

TRANSLUCENT BUTTON

5 [in] LOWER APERTURE

ALUMINUM RECTANGLE

ALUMINUM INSERT

Figure 17. Looking down from mirror 1 in tracker at aluminum

pieces and button used in lamp adjustment.

33
Spectral irradiance calibration . The standard lamp calibrations had to be frequent

enough and extensive enough relative to wavelength, tracker position and filters so that a sufficiently accurate calibration was available for any time, wavelength and measurement

configuration (tracker position or filter) for which solar data was taken.

Relative to time, calibrations were performed as often as practical, primarily whenever weather permitted. This turned out to be at least every other night during the

period in which good solar data were obtained. Successive calibrations taken about

48 hours apart differed by a maximum of a few percent. Relative to wavelength, standard

lamp calibrations were obtained between 340 and 280 [nm] at 5 [nm] intervals. Previous

experience had shown this to result in a least squares fit with a standard deviation of

the fit of a few tenths of a percent. To confirm that 5 [nm] intervals were adequate, one run was also taken at 1 [nm] intervals. To obtain the effect of tracker position,

the 340-280 [nm] runs were obtained for about every half hour of tracker position between

10:00 and 16:30 EST. Figure 9 is a typical example of a relative tracker calibration.

Though a complete calibration relative to the tracker was not performed every evening

during which calibrations were performed, sufficient data were taken to show any changes

in the relative tracker calibration over the eight days of data taking. No significant

change was detected. Sufficient standard lamp data were also taken with the neutral

density and solar blind filters and the diffuser to determine their transmittances and to detect any changes in their transmittances over the eight days of operation. None were

observed. The spectral transmittances of each of these optical elements were obtained in

the wavelength range in which they were used (neutral density filter and diffuser, 340-

305 [nm] ; solar blind, 296-287 [nm]). For optimum accuracy, it was necessary to obtain this transmittance with the same measurement beam configuration that was used in

taking the solar data (as opposed, e.g., to using a general purpose spectrophotometer to determine the transmittances) . This eliminated the need for a tedious characterization of

the filters and the optical beam relative to uniformity and direction.

Wavelength calibration . Wavelength calibrations were made every morning and late afternoon.

Five mercury spectral lines at 289.360, 296.728, 312.566, 334.148, and 365.015 [nm] from

a low pressure pen ray lamp were used. The lamp was used with a 5 [mm] aperture in

front of it and with the aperture at a distance of about 573 [mm] from the slit, so that

the largest plane angle subtended by that aperture at the slit was 0.5 [deg] . The mercury

lamp and its aperture were also positioned so that the path of this beam through the

monochromator was the same as that of the solar beam. As discussed earlier, the wavelength encoder readout for each scanned spectral line was taken to be the average of the

-2

readouts on each side of the peak where the signal was exactly equal to 10 that of the

peak (10 for the 289.36 [nm] line). To obtain an estimate of the wavelength hysteresis

effects that had been observed, wavelength calibrations were performed starting at about

289 [nm] and going to about 365.4 [nm] and then back to 289 [nm]

.

Wavelengths for each of the five lines were always obtained in a spectral scan that was decreasing in wavelength. This was the case even when performing calibrations starting

34
with the 289 [nm] line and ending with the 365 [nm] line. Each line in this sequence was still scanned in decreasing wavelength to minimize backlash errors. A typical calibration correction curve is shown in figure 18 where the difference between the published

wavelength of a line and the corresponding wavelength encoder readout is plotted against

wavelength. The largest wavelength hysteresis usually observed was 0.04 [nm] . The

dashed line in the figure, the mean of the calibrations in the two wavelength directions

(indicated by arrows), was used as the calibration for the time these wavelength data were

obtained.

Solar measurements . Solar data were taken in Gainesville, Florida between June 11, 1980

and June 18, 1980 whenever the sky was sufficiently clear. This meant that there were no visible clouds in the sun's line of sight. Four types of data were obtained for four

different purposes. These were (1) short wavelength cut-off data (287-296 [nm] at

1 [nm] intervals), (2) data for ozone determinations (294.7 - 305.2 [nm] at a sufficient number of wavelengths so that the spectral structure could be used to obtain at least 5 spectral irradiances for which the wavelength uncertainty was not greater than

0.01 [nm]), (3) data for ozone determination at the "Dobson wavelengths" (305.5 - 340)

[nm] and (4) data at various wavelength intervals of 0.1 [nm] to 2 [nm] over the

wider spectral interval of the solar spectral irradiance which would be required for

deconvolution calculations (295 - 340) [nm] . In all, eighty-one different experimental

runs were carried out.

The electronic components of the spectroradiometer were left on continuously for the

entire 8 days of data taking. The anode to cathode voltage on the photomultiplier was maintained at 1500 [V] . The discriminator voltage was set to produce a dark count rate

of about 0.3 [c«s ] .

Before starting an experimental run, a check was made to insure that the shadow of

the 3.25 [in] tracker aperture was concentric with the dif fuser/filter system. If the

shadow was not centered, it was made so by overriding the computer control of the tracker

stepping motors with a manually operated control. Next, the appropriate filter or diffuser cap was inserted and a computer program selected for one of the four types of data

runs. In order to observe, during each run, all parts of the spectrum under closely

similar atmospheric conditions and solar paths, integration times were limited to about

1 [s] or to that required to obtain about 10,000 [c] . An experimental run required

between 3 and 30 [min] with most of them about 5 [min] . In order to minimize this run

time, data being taken were usually stored on the computer disk, and a hard copy made at end of day. Continuous visual monitoring of the sun was maintained during the run to insure that no visible clouds were in line of sight of the sun. Notes were taken during

the experimental run describing environmental conditions and commenting on anything that

occurred that was considered potentially useful. As many of the measurements as possible

were made within one hour of high noon (^12:30 EST). When comparisons were to be made;

e.g., comparing the Dobson and "Sharp Cut-Off" ozone determinations, one type of run was made twice, and it bracketed the other type in time; and all runs were made in as short a 35
X

Wavelength

Hysteresis

X

Figure 18. Typical correction curve for the monochromator

wavelength readout. Maximum observed wavelength

hysteresis was about 0.04 [nm]

.

36
time as possible. In this way, atmospheric changes were less likely to occur during the

comparison, and if they did occur, would be more likely to be detected. Data taking was automatically interrupted via the computer program when a filter or diffuser had to be

inserted. Ambient temperature control was limited to manual control of window air conditioners but the air temperature near the monochromator was taken and automatically recorded

about once per minute. Barometric pressure readings were obtained continuously. Records

for the weather parameters such as humidity, visibility, temperature, and wind, taken each

hour, were available from the Gainesville Weather Station. Table 1 is an example of a typical computer printout of data obtained in one short run.

Table 1. Typical computer printout for a short run of data.

DATA FILE NAME- BrWSOLBl

DATE 6/18/80

TEMPERATURE 2 5.03 9 [°C]

TIME 11:51:25 EST

WAVELENGTH

296.002

295.000

294.001

293.002

292.002

TIME- 11:53:52 EST

291.000

289.998

288.998

287.999

287.000

TIME- 12:09:25 EST

PHOTON COUNT

319828

93692

52306

256625

119052

COUNTING RATE [cps]

159914.00

46846.00

26153.00

8554.17

3968.40

TEMPERATURE 25.097 [°C]

26241 874.70

17264 287.73

6177 51.48

1278 10.65

3029 5.05

TEMPERATURE- 23.030 [°C]

DATA REDUCTION and UNCERTAINTIES . Data reduction means obtaining the solar spectral

irradiance E, at the wavelengths of interest or the average of E weighted by the slitA A scattering function. In this problem, because the spectral slit width is so much greater

(0.18 [nm]) than the wavelength differences for which large changes occur in the solar

spectrum (<0.01 [nm]), we must be satisfied with a weighted average of E .

37
In reducing and analyzing the data, we start with the measurement equation, eq. (1.12),

S(A

Q

,t,T) C(S').S'U

o ,t,T)

J E

x (X,t).R

E

(X o ,A,t,T).d;

_ j AA

| E^(A,t).R

E

(A

o ,A,t,T

s ).d;

J A)

'AA

A _

" (1.18)

S

S (A

Q

,t,T

s

) C(S

,S )-S'S (A o ,t,T

s

)

where the independent variables A (wavelength setting of the monochromator) , t (time

at which S' was obtained), and T (tracker orientation indicated by time) have been

inserted to emphasize that the responsivity is a function of these variables. The irradiance responsivity may be written

R

E

(A

o ,A,t,T) = T(A,t)-z(Ao ,A,T).R^(A

o ,t,T), (1.19)

where t(A,t) is the spectral transmittance at time t of any filter, including the

diffuser, z(A ,A,T) is the slit-scattering function (p. 15, 910-4) [6] 1

, and R_(A ,t,T)

o bo

is the responsivity factor for tracker orientation T. When we substitute eq. (1.19) into

the measurement equation, eq. (1.18), we have

S'(A

o ,t,T) C(S'

S ).R^(A

o ,t,T).| E

A (A,t).x(A,t).z(Ao ,A,T)-dA

AA

S ,S(A ost,T ) C(S')-r£(A ,t,T ).[ E,(A,t).z(A ,A,T ) -d)

E o s 1 AA

. , A os

(1.20)

g where x for the case of the calibration signal, S' , has been set equal to one because

no filters were normally used in obtaining S' . The unknowns in this equation are

E. (A,t) and z. We have reliable measurements for the central part of z, approximately

A ±0.4 [nm] on either side of the peak, and we have an upper limit to the magnitude of z —8

at +50 [nm] from the peak. This is about 10 . Roughly sketching in the intermediate

values of z and then using this slit-scattering function in a simple deconvolution (p.

38, 910-4) [11] on spectral runs for which data were obtained to 287 [nm] , we found that

the computed scattering was about 100 times more than the observed signal count rate S' at 287 [nm] . The only explanation we have for this huge discrepancy is that the long

*In TN 910-4 [6], the slit-scattering function has the functional form z(A -A). It is

not necessary to restrict it to that form in this investigation, and we define it here more generally as

R

E (A,AQ

,t,T)

R|(X

o ,t,T)

z(A ,A,T) =

38
wavelength wing of the slit-scattering function for our instrument when observing the sun

— 1 —8

without a diffuser 1 is about 10 rather than 10 . Calculations show that with a slit-scattering function equal to 10 in the long wavelength wing, scattering would be

negligible down to 290 [nm] . This is experimentally confirmed by comparing S'(287),

which is about equal to or greater than the scattered signal at 287 or 290 [nm] , to S'(290). Since there is not enough power in the UV in available CW lasers to determine

the distant wings of z accurately, the lower wavelength limit for accurate data reduction is about 290 [nm] . And since scattering is insignificant for X > 290 [nm] , we may limit AX to only the central portion of z. Trial convolutions showed that it was

sufficient for AX to be equal to 0.44 [nm] ; that is, 0.22 [nm] on either side of the

peak of z.

For the wavelength range X ±0.22 [nm] , eq. (1.20) can be simplified as follows

X +0.22

o S'(X ,t,T) C(S

,S ).t(X ,t)-R!(X ,t,T)- f E.(X,t)-z(X ,X,T)-d

O O H O / A o

X -0.22

o

X +0.22

o (1.21)

S ,S

(X OS,t,T ) C(S')-E^a AOjiOSf .t).R!a .t,T )• /* z(X.X,T)-dX OS X -0.22

o

/

X +0.22

o E.(X,t)«z(X ,X,T)«dX

A O

/

X -0.22 C(S')-S'(X ,t,T).E^(X ,t)

r+7T22 s l >o^ = —:—

r

— (1 - 22)

X o+U ' ZZ A

,° C(S

,S ).S

,S (X OS,t,T )-t(X ,t).P

o z(X ,X,T )-dX

o s

X -0.22

o

where

f R|(X ,t,T.)

p = _JL_° (1.23)

is the polarization correction required when the calibration data S' are obtained with

tracker orientation T and solar data S' with tracker position T. Calculations

s involving eqs. (1.20) and (1.21) show that this simplification produces a negligible error

(<0.3 percent). From previous experience, we expect that the difference between z(X ,X,T

because the terrestrial sun is confined to such a small angle (0.5 [deg]), its irradiance

on the entrance slit of the spectroradiometer is highly coherent. Calculations of the

type described by Shumaker [26] show that for the f/5 spectroradiometer that we used the

distant wings of the slit-scattering function could be reduced by this order of magnitude.

39
and z(A , A,T ) for A ±0.22 [nm] is small, and we assume the effect of this difference

in eq. (1.22) is insignificant.

All the data and the equations resulting from the various fits were stored on floppy

disks. It was therefore a simple matter to write a program to compute E, (A ,t). This

-z

X ° was done and E was computed for all wavelengths in the 81 experimental runs. Examples

A of the data and results printed out from these computations are shown in tables B-l through

B-7, in Appendix IB. Keep in mind that these results have not been corrected for scattering. However, we believe this to be significant only below 290 [nm] . Also, they

have not been corrected for possible differences between using and not using a diffuser,

which will be addressed later.

In order to estimate the uncertainty in our determination of E [eq. (1.22)], we

A shall address the way in which each independent and dependent variable in this simplified

equation was obtained.

The first variable is A , which is the (corrected) wavelength setting of the spectro

radiometer. This is actually the peak or center wavelength of our slit-scattering function.

The wavelength calibrations that were taken every morning and late afternoon, one of which

is shown in figure 18, were generally used to obtain A . The data represented by the

dashed curve in the figure was fitted to a cubic equation in A . A linear interpolation

in time between the morning and afternoon calibrations was used to determine the wavelength correction at any time t. These wavelength calibrations were estimated to have an uncertainty ranging from ±0.02 [nm] at 290 [nm] , ±0.03 [nm] at 295 [nm] , ±0.03 [nm] at 305 [nm] to ±0.02 [nm] at 340 [nm] . A smaller wavelength uncertainty, estimated to be ±0.01 [nm] , was obtained in the data taken for ozone determinations by using the

spectral structure shown in figure 4. In this case, during a solar run, about five data

points were taken at 0.02 [nm] intervals through 5 or 6 of the troughs in figure 4. The

observed trough wavelengths were then compared with those obtained by convolution of

—

z

E (A,t), where E (A,t) was obtained in the manner described in Appendix A. The E

A A A uncertainties associated with these various wavelength uncertainties vary with wavelength

and are shown in table 2 along with the other uncertainties to be discussed in this section.

. The time (Eastern Standard), t, was provided by a clock in the computer and was

accurate to about one second. Time was stored along with the data at intervals of about one minute. The time parameter was used to compute the orientation of the tracker for

polarization corrections and for linear interpolations of the standard lamp calibration,

S' and introduced negligible uncertainty in E.. . A The signal counting rate, S', for solar photons was obtained with an integration

time varying from one second to 10 minutes, chosen to realize a standard deviation for S' of 1 percent or less. In photon counting, the standard deviation of the signal is

approximately equal to the square root of the total counts. The dark count rate was always set to about 0.3 [cs ] by adjusting the discriminator voltage and was subtracted from the observed signal rate when significant. Time intervals for integrations

40
3

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cfl 3

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l-l cr CO

cfl cfl 3 H 3 X)

cfl cr 4-1 •H

4J CO o > oH

41
were determined by the computer with negligible uncertainty. Time was the basis for

automatic control of the tracker orientation such that the solar beam remained centered

relative to the entrance slit of the spectroradiotneter. This automatic mechanism malfunctioned rather frequently during the runs, requiring manual control. We have assigned

a 2 percent uncertainty for this malfunctioning as indicated in table 2.

The correction C(S') (for not being able to resolve all the photon counts) given in

eq. (1.15b) is considered uncertain by about 1 percent for counting rates from

5 x 10 [cs ] to the highest observed. At lower counting rates, its uncertainty is

estimated to decrease monotonically to a few tenths of one percent at 10 [cs ].

The spectral irradiance of the 1000 [W] frosted tungsten halogen standard Ef(X,t)

A was obtained by a comparison calibration with three NBS spectral irradiance 1000 [W]

standards before and after the eight-day period of solar observations. This was performed

at the normal distance of 50 [cm] and at 5 [nm] intervals for the wavelength range

280-350 [nm] . No significant change was observed in the two calibrations obtained 8 days

apart. The spectral irradiance of the frosted lamp at the distance used, 396.3 [cm]

without diffuser and 384.8 [cm] with diffuser, was calculated assuming an inverse

square law dependence relative to 50 [cm]. From previous experience, the uncertainty of

this procedure for obtaining E of this type lamp at the above distances does not exceed

0.5 percent. In order to obtain the spectral irradiance at wavelengths other than the

5 [nm] intervals at which data was taken, a least squares fit was performed to the expression

E*(X) = <A

X + A

2 -X + A

3 -X

2 + A

4

-X

3 + A

5 .xVx"5 -e [a+(bA)]

(1.24)

s 2 with weights of 1/(E?) (NBS Tech Note 594-13) [13]. If only a linear least squares

computer program is available, one can determine the quantities a and b from a fit of

Hn(E®.X5

) - a + (b/X) (1.25)

with weights of 1. Then with a and b determined, one obtains the A from a fit of

s 2 s eq. (1.24) with weights 1/(E.). The uncertainty of E at the distances and wavelengths used in this experiment is estimated to be 3 percent.

g The standard lamp calibration data S were obtained as a function of wavelength by

fitting an equation similar to eq. (1.24) but without the cubic and quartic terms (these

s s terms were not significant in the S fits) and with a weighting of l/(At«S ) where At

is the integration time in seconds. In linear least squares fitting, the weights are

4 proportional to the reciprocals of the variances. Total counts varied from about 10 [c]

at 280 [nm] to 3 x 10 [c] at 350 [nm] when an integrating time of 5 [s] was used

(no filters or diffuser) . Fits performed with both 1 [nm] and 5 [nm] interval data

42
demonstrated that the 5 [nm] interval spacing was sufficiently close. Successive calibrations taken 48 hours apart differed by a maximum of about 2 percent which was attributed to imprecision (noise), alignment errors, and changes in the tracker mirrors. The

calibration used for any particular solar measurement was obtained by linear interpolation,

with respect to time, between the 48-hour calibrations. The uncertainty of S was estimated to be 2 percent as indicated in table 2.

Spectral transmittance data of the solar blind filter and diffuser were fitted with a quadratic function of wavelength with an insignificant (<0.5 percent) standard deviation

for the fits. The solar blind filter had significant non-uniformities and the reproducibility in positioning this filter was about 2 percent. This problem did not exist for the

diffuser. The neutral density filter had a constant transmittance as a function of wave- length to within the precision of the measurements of 1 percent. It did not possess

significant non-uniformities. None of the filters showed any change in transmittance over

the five nights of calibration. There was no reason to expect the solar blind or neutral

density filter to be dependent on tracker orientation, and this was confirmed experimentally. Since the output signal of the spectroradiometer was not a function of tracker

orientation with the diffuser in place, but without it, the output signal did vary with

tracker orientation, the effective transmittance of the diffuser was always determined

relative to one particular tracker orientation. This was taken to be the orientation at 12:30 EST. The uncertainties assigned these filters were 3 percent for the solar blind

filter, 2 percent for the diffuser, and 1 percent for the neutral density filter.

The polarization correction for tracker orientation was obtained by two quadratic

spline 1 "fits." The first fit was used to interpolate relative to tracker orientation for

each of the 5 [nm] lamp calibration data. Since Rp(^ >t,T ) is proportional to

*A spline "fit" is a manner of interpolating non-linearly between a large number of data

points. The procedure is to determine the coefficients of an nth order (usually n = 2 or 3) polynomial that "goes through" the first n + 1 data points, then the coefficients

of the same order polynomial that "goes through" the second to n + 2 data points, and so on until all the data points are used. Then these polynomials are used to calculate the

interpolated values. Since two or more polynomials can be used for calculating the same interpolated point, a standard format is set up which selects a particular polynomial.

For example, if n = 3, a typical format would be to use the first polynomial for interpolating between the first 3 data points and the last polynomial for interpolating

between the last 3 data points. Each of the remaining polynomials is used for interpolating between the 2nd and 3rd point used in determining that polynomial. Once a computer program has been written to accomplish all this, it is a simple, fast procedure

to carry out. We have often used spline "fits" when we wanted data at equal intervals of

the independent variable but the data wasn't taken at these intervals, and we did not know

an appropriate equation to use for a least-squares fit.

43
S' (A ,t,T ) OS • C(S' ), these data could be used to interpolate relative to the 10:00 to 17:00 tracker orientations (T) . Curves similar to that shown in figure 9 were computed

and stored on a floppy disk for each of the 5 [nm] runs from 340 to 280 [nm] . The

tracker polarization correction P eq. (1.23) was determined by obtaining the ratio

S ,S

(Xo ,t,T)

S ,S (Ao ,t,T')

where T is the tracker time for which the particular solar data S' was obtained and

T' is the closest tracker time to T for which a lamp calibration was obtained. These

ratios were determined for each of the 5 [nm] data and a 2nd quadratic spline fit was performed as a function of wavelength, The uncertainty of P was estimated to be 2 percent.

In order to detect any changes or drifts with respect to time in the spectroradiometer

responsivity function, the standard lamp was set up in the laboratory and observed each

morning before solar measurements began and in the late afternoon after solar measurements

for that day had ended. The major differences between these lamp observations and the

roof calibrations were that the former did not include the tracker and did not have to be

made at night in an outdoor environment. These made the "lamp observations" more precise

and they could be obtained more frequently. In order that corrections C(S') for high

count rates be negligible, the neutral density filter was employed. Figure 19 is a plot

of these results and the roof calibrations (S' ) for 330, 335 and 340 [nm] . The

"inside-laboratory" calibration had the same long-term drift as the roof calibration.

However, short-term changes were different. We do not know the reason for this, but it is

conceivably due to laboratory temperature changes. We attributed an uncertainty of 2 percent to this effect, referring to it in table 2 as "linear interpolation relative to time of roof calibration".

As mentioned earlier, we had planned to take several sets of data at the longer

wavelengths with and without a diffuser to determine directly any differences between

these two approaches. The set of runs 42, 43, and 44 in tables B-5, B-6, and B-7,

respectively, is one such example. All these comparisons showed that there was a difference

of about 5 percent, independent of wavelength, between the "diffuser" and "no-dif fuser" runs with the latter resulting in higher values of spectral irradiance. We have not been

able to determine the cause of this difference, but our suspicion is that it is due to differences in the beam geometry of the sun and standard lamp and lack of sufficient

uniformity in the flux responsivity. We believe the diffuse data is correct and therefore

must reduce all the data taken without a diffuser (virtually all below 305 [nm]) by the

5.3 percent difference observed. This correction has not yet been applied to the nondif fuser data in tables B-l to B-7 in Appendix IB. The uncertainty of such a correction

44
CDCD

C

_c

u

-p

c

(D

L

CD CL

2 -

-2 -

-4

© Lamp on roof

* Lamp on roof with N. D. filter

a. Lamp in lab with N. D. filter — Values used in data reduction

6-11 6-12 6-13 6-14 6-15 6-16 6-17 6-18

Date

Figure 19. Change with time of direct mode lamp calibrations (S' ) for 300, 335, and 345 [nm] data.

45
has been estimated, from the precision of the dif fuser/no-dif fuser comparisons, to be

about 2 percent. This is the last item in the uncertainties of table 2.

It is common practice to make an estimate of the overall or total uncertainty of

experimental measurements by combining in quadrature (square root of the sum of the squares)

all the individual, independent uncertainties such as those listed in table 2. This has

been done, and the result, given at the bottom of table 2, varies from 7.4 percent at short wavelengths to 5.7 percent at long wavelengths.

There are applications of solar terrestrial spectral irradiance measurements where

only the ratio of values at wavelength intervals of 2 or 3 [nm] are needed. Many of the

uncertainties in table 2 are significantly less for such relative spectral measurements,

particularly when the data from which the ratio is to be determined have been obtained in

time intervals of a few minutes. We estimate that the total uncertainty for such relative

spectral measurements is about 3 percent or roughly half that shown in table 2. The

component uncertainties contributing to this smaller uncertainty are wavelength—2 percent, noise (S') —1 percent, C(S') —1 percent, noise (S' ) —1 percent, E.. —1 percent,

A and polarization—1 percent.

The repeatability of non-diffuser experimental runs taken at 10 to 30 minute intervals

is not as good as predicted by our uncertainty estimates. Comparing such data when viewing

conditions were good and wavelength uncertainties negligible, we found systematic differences that averaged 4 percent in successive runs. We did not see this large a difference when the dif fuser was used. However, we only had one appropriate set of diffuser

runs for checking this repeatability. In this case, there was a difference of only

1 percent. The only factor of which we are aware that could cause the lack of repeatability of 4 percent for the non-diffuser runs is improper alignment relative to the peak

of the responsivity function (see figure 8). In this case, systematic errors of about

1/2 deg in solar tracking during a run would account for the results observed. The

tracking malfunction uncertainty in table 2 addresses this type of behavior. However, the

amount assigned this uncertainty (in table 2) accounts for only half the non-repeatability

observed, and we wbuld expect this uncertainty to reflect itself in a somewhat less

systematic manner. As a result of this unaccountable behavior of our data, we add another

2 percent uncertainty to the totals in table 2 resulting in about 10 percent at the

short wavelengths and 8 percent at the long wavelengths.

The question arises of whether or not a significant reduction of uncertainty in these

solar terrestrial spectral irradiance measurements is likely without a major improvement

in the spectroradiometer and standard. We believe the answer is yes if the existing

mirror tracker were eliminated and the monochromator were located on the roof and itself

mounted on a very accurate solar tracker. Arrangements also would have to be made for

proper temperature control of the spectroradiometer. With such an arrangement, the solar

tracking malfunction uncertainty, the systematic differences referred to in the last

paragraph, the polarization correction and its uncertainty, and half the uncertainty

associated with the standard lamp signal S' would be eliminated. In addition, we

46
believe the uncertainty associated with the lack of uniformity of the filters and with

their transmittance measurements could be reduced by a factor of about two. Furthermore,

whenever possible, one should use a diffuser. This is no problem for wavelengths greater

than 305 [nm] . Between 295 and 305 [nm] it is possible only when integration times of

100 to 10 [s], respectively, can be employed. In all, it should be possible to realize a total uncertainty as computed in table 2 of about 6 percent at 290 [nm] and 4 percent

between about 300 and 340 [nm]

.

FUTURE INVESTIGATIONS . There are three investigations or areas of research to which we would give a high priority in any future efforts in UV solar terrestrial radiometry.

The first investigation is a direct test of the effect of coherence of the solar flux

on spectral scattering. We found negligible scattered signal at 290 [nm] which we attributed to the high coherence of the flux when the sun itself and the entrance slit

-4 defined the solar beam (solid angle at entrance slit of approximately 10 [sr]). This reason for the low scattering could be confirmed easily by first spectrally scanning

between 295 and 290 [nm] with a low scattering, double monochromator under our viewing

conditions and, immediately afterward, performing another scan with an appropriate lens

inserted so that the entrance slit was irradiated with a much larger solid angle (e.g.,

the collimator of an f/5 instrument being filled or a solid angle of approximately 0.03

[sr]). If coherence is responsible for the significantly lower scattering, S(295)/S(290)

from the two scans should differ by a factor of between about 50 and 100.

The second area of research in UV solar terrestrial radiometry that we believe should

receive high priority is extending the measurements of the sun itself described in this

chapter to measurements of the sun and sky; that is, hemispherical viewing. In the UV,

the solar terrestrial hemispherical spectral irradiance is about twice that of the spectral irradiance of the sun itself [14]. Ultraviolet measurements of the sun itself, as described in this chapter, are of major interest for ozone and aerosol determinations.

Hemispherical measurements are of interest in studies of biological effects. The usual

way in which hemispherical measurements are made is with a diffuser that obeys the cosine

law. Development and accurate characterization of a suitable diffuser would constitute

3 the major effort in this investigation. Because of the signal attenuation of about 10

when using a diffuser, measurements will probably not be practical below about 292 or 293

[nm] . Even down to these wavelengths, the spectral slit width will have to be increased to

2

1 [nm] and the entrance slit area to about 1 [mm ]. Because the ratio of hemispherical

spectral irradiance to solar spectral irradiance changes orders of magnitude less relative

to wavelength than the hemispherical quantity itself [14], the direct measurement of the

ratio should be considered. If the need for going to shorter wavelengths is sufficiently

great, development of a lens or optical system capable of hemispherical viewing and cosine

law response might be attempted. Even if this were successful and the signal/noise problem

down to 290 [nm] were solved, the difficult problem of accurately correcting for scattered flux would remain.

47
Finally, any extensive research in UV solar terrestrial radiometry should consider an instrument in which the spectral irradiances at all wavelengths of interest can be measured

simultaneously. Changes in atmospheric conditions, often in a relatively short time, make

this feature highly desirable. Fourier transform spectroradiometers, multi-channel spectroradiometers, and spectrographs are obvious examples. However, in order to make accurate

measurements below about 300 [nm] , this instrument must have a slit-scattering function

comparable to that of a high quality double monochromator, and, to the best of our knowledge, this has not yet been realized.

SUMMARY of CHAPTER 1 . This chapter addresses the difficult problem of measuring the

solar terrestrial spectral irradiance from about 290 [nm] to 340 [nm] . It includes an account of the experimental design and measurements that were carried out in Gainesville,

Florida, in June 1980. The major reasons for these measurements were to (1) apply current

state-of-the-art radiometric instruments and techniques to UV solar terrestrial measurements

and present the results in this Manual as a first applications chapter and (2) explore

the potential of using solar data at wavelengths below 305 [nm] for determining atmospheric ozone thicknesses. Item 1 is the subject of this chapter. Item 2 is being developed

for submission to Applied Optics.

The chapter begins with estimates of the spectral irradiances of the sun (not including sky) as seen from the surface of the earth. These are calculated using the equations

developed in Appendix 1A. The results of the calculations are shown in figures 2 through

4. Figure 3 shows that with a spectral slit width of 0.003 [nm] considerable spectral

structure appears. Therefore if spectral slit widths of 0.1 [nm] to 1.0 [nm] are used,

as is common in radiometry, the measurements will provide only a weighted average spectral

irradiance, weighted by the slit-scattering function of the spectroradiometer.

The measurement configuration that we used in this problem is shown in figures 5 through 7. The advantages of the common practice in irradiance measurements of using a diffuser as the first element of the spectroradiometer are reviewed. However, a signal

reduction factor of about 1000 makes the diffuser impractical to use below about 305

[nm] where measurements for ozone determinations are to be concentrated. It is demonstrated that if a diffuser is not used, the flux responsivity function must be sufficiently

uniform over the angular extent of both the sun and the lamp standard used in calibrating

the spectroradiometer.

The general measurement equation for incoherent radiation (p. 23, 910-3) [9],

S(X

o

) = J J

(R00* L + R01' L

1 + R02* L

2 + H

03

.L

3 ).coBe.d».dA: 4A (1.3)

^X J AAJ Aw

is applied to viewing both the sun and the standard lamp resulting in

48
S(X

q

) 4<VT) • E

A .z(Xo ,X,T).dA

SS( V 4<W • f E

X- Z(X

o'

A ' T

s

)

- d

J A)

AX (1.13)

AA

where R

e

(A o ,T) is the irradiance responsivlty factor at wavelength A and tracker

orientation T; and where z is the slit-scattering function (p. 15, 910-4) [6].

The estimated irradiances, measurement configuration, and measurement equation are used to arrive at the specifications of the monochromator required for these measurements

so that their uncertainty is less than 10 percent. These include a wavelength uncertainty

of 0.01 [rim] or less, spectral slit widths varying from about 0.2 to 1 [nm] , very low

—8

(<10 ) wings on the slit-scattering function and as large a geometrical throughput as available. A block diagram of the complete spectroradiometer selected is shown in figure

5, and detailed specifications for the instrument are also presented.

In order to minimize errors in the radiometric measurements, the flux responsivity of

the spectroradiometer is characterized for the parameters for which a significant difference exists between the spectral irradiance of the sun and that of the lamp used as a calibration standard. The parameters involved are magnitude of the flux and spectral

distribution.

For magnitude, the following correction to the output signal is experimentally

obtained:

|r = C(S*) = 1 + 6.927-10" 8

-S' + 7.174-10

_15

-S'

2 (1.15b)

where S is the "corrected" output signal and S' is the output signal actually observed.

The rapid fall-off in solar terrestrial spectral irradiance below 305 [nm] and the

extensive structure require a maximum wavelength uncertainty of about 0.01 [nm] if wave- length accuracy is not to be a significant factor. It is found that this 0.01 [nm]

uncertainty is realizable with this best available portable instrument only by using the

spectral structure of the sun itself in a wavelength self-calibration while taking solar

data. In order to obtain the calibration wavelengths in this observed spectral structure

(by evaluating eq. (1.13) as a function of wavelength) the central portion of the slitscattering function is required. It is obtained from spectral scans of various mercury

and laser lines.

—8

An accurate determination of the distant wings (to values of 10 or less) of the

slit-scattering function is required in order to perform a deconvolution of eq. (1.13) to obtain a correction for scattering. This has not been possible because of insufficient

power (<< 10 [mw]) in available lasers. However, an estimate of the required long wave- length wing has been obtained using the strong 253.7 [nm] mercury line. The result is

—8

2*10 at 53 [nm] from the peak, with an uncertainty of about a factor of two.

49
The detailed manner in which the solar measurements were made is presented. This

included an accurate optical alignment using a laser (required because a diffuser was not

used for most of the measurements) , frequent spectral irradiance and wavelength calibrations, selection of integration times and total time for experiments, visual monitoring,

temperature control, weather conditions and computer usage, including control. Four types

of data were obtained. These consisted of (1) sharp ozone cut-off data (A < 295 [nm]),

(2) data for the new-type ozone determinations (295 < A < 305) , (3) data for Dobson type ozone determinations (305 < X < 340), and (4) data required for performing convolutions.

Examples of these four types of data are shown in tables B-l through B-7 in Appendix IB.

For reducing the data and estimating the uncertainty of the measurements, the measurement equation is reduced to

/

A +0.22

oE,(A,t)-z(A ,A,T)-dA

A o

/

A -0.22 C(S').S'(X .t,T).E?J(A ,t)

rrcTr? s KiK'V = —:—r — • (1 - 22) o

- 22 A ° C(S

,S ).S,S

(A o ,t,T

g )-T(Ao ,t).P

z(A ,A,T )«dA

o s

A -0.22

o

where f BjjCX .t.Ti)

P = -f-2 (1.23)

g is the polarization correction required when the calibration data S' are obtained with

g tracker orientation T and solar data S' with tracker orientation T. E^ is the

s A spectral irradiance of the standard lamp as used in the calibration and t is the transmittance of any filters inserted in the optical path for solar measurements but not inserted

for the lamp calibrations. The manner of obtaining each independent variable in eq.

(1.22) and its uncertainty is discussed. These uncertainties are summarized in table 2. Measurements made at wavelengths greater than 305 [nm] , where it is possible (with good

signal-to-noise ratio) to use a diffuser, showed a difference of 5.3 percent between

using and not using a diffuser. The diffuser data are believed to be more accurate, and

therefore all non-diffuser data will be corrected (multiplied by 0.947). This correction

has not yet been made for the data shown in tables B-l to B-7 in Appendix IB.

Spectral scattering is found to be insignificant down to 290 [nm] . This requires

the distant wings of the slit-scattering function to be about 10 . It is believed

that this value was realized in our non-diffuser measurements because the irradiation of

the slit of the monochromator, in this case, was quite coherent.

50
The uncertainty associated with each dependent and independent variable in eq. (1.22)

is discussed and estimated. The overall or total uncertainty is obtained by taking the

square root of the sum of the squares of the individual uncertainties in table 2. This

total uncertainty varies from 7.4 percent at the short wavelengths to 5.7 percent at 305 [nm] and longer wavelengths.

Comparison of a number of experimental runs shows that the repeatability is not as good as the uncertainty estimates predict. An additional uncertainty of 2 percent is

added to the totals given above to take account of this.

Means that can be taken to reduce these uncertainties are discussed. An improvement

of about one third is considered feasible if the mirror solar tracker can be eliminated

and the monochromator itself mounted on a precision solar tracker.

In some applications in which these measurements will be used, only ratios of solar

terrestrial spectral irradiance at wavelength intervals of only 2 or 3 [nm] are required.

These are estimated to have much lower uncertainties — about 3 percent.

Various suggestions are made for further research in UV solar terrestrial spectral

irradiance measurements. These include (1) direct confirmation of the effect of coherence

on scattering, (2) extension of the solar measurements to include global (sun plus sky)

measurements, and (3) the development of an instrument in which data for all wavelengths

of interest are obtained virtually simultaneously.

51
Appendix 1A (Part III)

Computation of Solar Terrestrial Spectral

Irradiance between 280 and 310 [nm]

^he purpose of this Appendix is to present our currently recommended procedure for com- puting the solar terrestrial spectral irradiance in the 280 to 310 [nm] region. It should be emphasized, however, that the accuracy of this recommended procedure has not yet

been critically evaluated.

52
In irradiance calculations, as in most calculations involving radiometric quantities,

there is less chance of error if one begins with the quantity radiance. The solar

spectral radiance at the earth's surface, L , is equal to the product of the solar specA tral radiance outside the earth's atmosphere (extraterrestrial) L^ and the spectral

A transmittance of the atmosphere x(X) along the path associated with this radiance

(p. 38, 910-1) [15]; that is

L, = Lf»T(A) [W-m"

2 -sr"1 .nm"

1

]. (A-l)

A A

The two spectral radiances in eq. (A-l) are shown in figure A-l along with the major

constituents of the atmosphere — ozone, aerosol, and air — that absorb or scatter the

solar flux in the region between 280 and 340 [nm] . The spectral transmittance asso- ciated with each of these constituents is, by the familiar exponential law of transmittance,

-q. (X) -seq .9 x.(X) = e

X (A-2)

where q.(X) is the optical depth1 of the i constituent for a vertical path (zenith

angle 0=0). Seq.0 is the ratio of the length of the actual path of the direct solar

flux to that of the vertical path. The optical depth q. can also be written as -3-1 1

2 n.a.W. 11111 or k.W. where n. [cm -atm is the number density, o. [cm ] is the attenl l _i_i

uation (or absorption) cross section, W. [cm«atm] is the thickness, and k. [cm «atm ] is the attenuation (or absorption) coefficient. 2 The overall transmittance, x(X), of

the atmospheric model .shown in figure A-l is

^he usual symbol for the optical depth in the literature on atmospheric optics is t. However, we have already used x throughout the rest of this Manual for transmittance.

Accordingly, we have adopted here the symbol q for optical depth, writing q.(X)

instead of x.(X). Incidentally, don't confuse this with the unit of photon flux, the

quantum [q], which we always enclose in square brackets, as with all unit-dimension

symbols.

2 The CIE-IEC International Lighting Vocabulary (3rd ed.) calls this the linear attenuation

(or absorption) coefficient.

53
SUN

OZONE (q 3

)

AIR (q.,)

AEROSOL (q 2)

EARTH'S SURFACE

Figure A-l. Simple model of earth's atmosphere showing the major constituents that

absorb or scatter solar flux in the UVB and the solar terrestrial

spectral radiance L and solar extraterrestrial spectral radiance L , A A q. is the vertical optical depth of the ith constituent.

54
-q.-'seq-.U -q *seq„« -q„«seq_0

x(A) = t

1 (A).t2 (A).t

3 (A) = e -e -e (A-3)

-(q

1 'seq1

6 + q«seq

2

8 + q.-seqJ) (A-4)

t(A) = e

and substituting eq. (A-4) into eq. (A-l) , we obtain

-(q

1 «seq1

9 + q

2 «seq2

8 + q^seq.^)

L

A = V6

' (A" 5)

where q1

, q„ , and q_ represent the vertical optical depth for air, aerosol and ozone,

respectively.

To obtain the solar terrestrial spectral irradiance E. from the solar terrestrial

A spectral radiance L^ we apply the equation (p. 12, 910-2) [16]

E = / L •cos6' -do) (A-6)

to the configuration shown in figure (A-2) . Since 9' does not exceed about 0.25 [deg]

,

E = /V/ L, -dco (A-7)

U)

to a very high accuracy. Substituting the expression for L in eq. (A-5) into eq. (A-7), we obtain

-(q

1 «seq].e + q -seq^ + q3 «seq

3

9) E = | L «e «dcj. (A-8)

" /

Since each of the q. and seq. 8 vary only slightly over m

i

-(q -seq 6 + q -seq G + q^seq^) . _ 2 E, = e • / L -dco [W«m «nm J. (A-9)

A

• -'A /*.

The solid angle u> subtended by the sun at the earth's surface is insignificantly different

from that subtended by the sun at the top of the earth's atmosphere. Therefore

-(q -seq 9 + q,-seq 8 + q_-seq 9) E = e X L 12- J J , E

e (A_ 10)

A A

55
SUN

APPROX.

0.5 [DEG]

SURFACE OF IRRADIATION

NEAR EARTH'S SURFACE

Figure A-2. Geometry involved in relating, through eq. (A-6)

,

the solar terrestrial spectral radiance and solar

terrestrial spectral irradiance.

56
where E. is the solar extraterrestrial spectral irradiance and E, is the solar terresA A trial spectral irradiance.

The expression that we have used for the vertical optical depth for air q.. is [17]

1.0456'P /300\4 0.1462-(300/X) 2

, t

• q

l = 1013 '{—) ' e (A-U)

where P is the atmospheric pressure in millibars [mb] at the point for which E. is

A being determined and X is the wavelength in nanometers [nm]

.

The vertical optical depth for aerosol q for the limited range of 290 to 340

[nm] may be expressed [3] as

q

2 = q20

- s 20 -(x-3oo) (a-12)

where q and S„_ are constants. The constants used in the computation of E in

figure 2 through figure 4 were representative values obtained in our 1980 Gainesville

measurements (q„ n = 0.5 and S„

n = 0.0033 [nm I). 1

The vertical optical depth for ozone q_ may be written

q

3 (y) = k

3 (y)-W3 (y) (A-13)

where k_(y) [cm «atm ] is the ozone absorption coefficient and VL(y) [cm*atm] is the ozone vertical thickness at a point at an altitude y [km] where E is being computed.

A The absorption coefficient k~ is also a function of temperature. At wavelengths between

245 [nm] and 311 [nm] , which includes the wavelengths with which this investigation is

primarily concerned, this functional dependence is not great and may be represented by [17]

k

3 (X,t) = k3 (A,t

o ).[l + |[(t-t

o )/642] + [(t-t

o )/395]

2 }-e (A -300)/4 °] (A-14)

where t and t are in degrees Celsius [°C] and X is in nanometers [nm] . For our calculations, values of k~(X,t ) were obtained from measurements by Bass [18].

To take account of the variation of k, in the earth's atmosphere due to the variation of ozone temperature and number density, the following procedure was followed. A

differential element of ozone optical depth dq_ at an altitude y where the temperature

is t may be written as

^hose interested in how q„ may vary for different types of aerosols and in analytical

expressions covering a much larger wavelength range are referred to Green and Schippnick

[17].

57
dq

3 = k

3 (t)-dW3 (y). (A-15)

The total ozone optical depth is

•i

W

3 (y)

q

3 = k3 (t)-dW3 (y), (A-16)

where W_(y) is the thickness of ozone above altitude y. In eq. (A-16) we are integrating from the top of the atmosphere (y = °°) where W_ = to a point in the atmosphere where the altitude is y and ozone thickness above y is W.(y). If W is the

total thickness of ozone W = W (0) and N(y) is the fraction of this thickness above

altitude y,

dW

3 (y) = W3Q

.dN(y) = W^-^Vdy (A-17)

and from eq. (A-16)

.N(y)

q

3 (y) = k3 (t)-W

3Q

-dN (A-18)

I

q

3 (y) k3 (t).W

30 .p.dy. (A-19)

Substituting eq. (A-14) into eq. (A-19), we obtain

q

3 (y) /'[l + {[(t-t„)/M2] + [(t-t

o )/395]

2 }.e ( *-300)/40

]. k3(t

o

,

•«30-fK

q

3

oo

(y) - -k3 ( to ).W

30 .J"[l + {[(t-t

o )/642] + [( t -to )/395]

2 }.e"-3(' »/ 4

°]

fK

58

(A-20)

(A-21)
The total ozone optical depth q,.(0) which we designate simply q„ is

q

3 (0) -W^o-jJ dy

+ /{[<t-t >/642] + [( t -

to )/395]

2 }.e^-30

°)^.(f).dy]

(A-22)

q

3 = -k3

(t o ).W

30

-

_ 00 _ -1 + ^-W">.j |[( tto )/642] + [( t -t

o )/395]

2 }.(f).dy

I. (A-23)

For ozone, N(y) may be written [19]

N(y) = 0.1307 0.9709

2.350 +ey /2 ' 66 1+e (y-22.51)/4.920

(A-24)

where the altitude y is in kilometers [km]. Differentiating eq. (A-24), we obtain

dN 0.04914-e

dy

y/2.66 0.1973-e (y-22.51)/4.92

(

2 .350 + e^

/2 - 66

) (l + e (y-22.51)/4.92)'

(A-25)

and substituting this into eq. (A-23)

, t^ -v t, [-, , n (X-300)/40|

q

3 = k3 (t o ).W30 .[n-C.e^

J (A-26)

where

C = /

{[tt-V 7642] + [Ct-^ )7395j

2

}

,,.37/2.66 o. 197 3.e^-22 - 51 ) /4 - 92 —nz\1 *dy. (A-27)

(2.350 + e^ /2 ' 66

)

2

( 1+e(y-22.51)/4.92)

:

The constant C may be numerically evaluated for a particular t using tables giving

atmospheric temperature t as a function of altitude y [20] . These tables depend on the

latitude and the time of year (month). For T = 18 [°C] and a latitude of 30°N in

o

59
July, C = -0.0714. For the same latitude but the month of January, C changes only

slightly to -0.0745. For T = 25 [°C] and a latitude of 30°N in July, C = -0.0762.

For A < 310 [nm] , the absorption coefficient for ozone at a particular temperature

t may be approximated by the expression [17]

k

3 (t o'

X) =

Q /(A-300)/Y ? (A"28 > p + e

Performing a non-linear least squares fit of Bass' data [18] from 288 to 305 [nm] to this

expression results in

a = 11.1419

6 = 0.04928

y = 7.1231

where k~(t ,A) has the units of [cm -atm ].

Expressions used for seq.6 . in eq. (A-10) are [21]

seq^e.y.) = fl - ^_1 J (A_ 29j

where

r. = [1 + (y i /R)]

2

, (A-30)

and where is the solar zenith angle, R [km] is the earth's radius (6371 [km]) and

where y. [km] is the effective altitude for the ith species. We used [21]

S

y (air) = 5.69 [km]

y„ (aerosol) = 1 [km]

y„(ozone) = 23.5 [km].

For small 6, seq,n (0.,y.) = secant 6.. The difference between seq. and secant is not

i l'-'i l l significant except for very large zenith angles. Even at = 58 [deg] , the difference

for the case of ozone is only 0.9 percent which amounts to a difference in computed E

A from eq. (A-10) of about 1 percent at 304.6 [nm] and 3 percent at 294.5 [nm] . For

air, the difference between using seq0 and secant at = 58 [deg] is about 0.2

percent which amounts to about 1/2 percent in E in this same wavelength range.

60
The remaining quantity required to compute the terrestrial solar spectral irradiance

E^ is the extraterrestrial solar spectral irradiance E

e

. We needed high spectral reso- lution (AA << 0.2 [nm]) data for E in order to determine the effect of instrumental

spectral slit widths equal to or much larger than 0.2 [nm] . High resolution E

8 data

A could not be found for the spectral region of interest. However, high resolution

(AA = 0.003 [nm]) L^ data were available for the solar center and one portion of the

solar limb [22]. These L^ data were used to calculate E

8 in the following manner. We

start with the relationship between spectral irradiance and radiance in eq. (A-6) . As

before [eq. (A-7)], for the case of terrestrial solar spectral irradiance, this becomes

/

L •dto, A (A-7)

SUN

APPROX. <(>

L°«t»

L

6

X (0)

Figure A-3. Configuration for computing solar extraterrestrial spectral

e e irradiance E from solar extraterrestrial spectral radiance L . A A

The solid angle dw subtended at the earth's surface by the annular ring of area

2-n-r-a-d$ [see figure (A-3)] on the sun's surface is

2TT'r-a»d<j)' costfr R

2

2TT»a »sin(|)'d(j) -costj

R

2 (A-31)

where R is the distance from the sun to the earth. Substituting this dw in eq. (A-7) we obtain

61
-(f)

2 -}

it/2

E® = 2ir« (-|) • I L® -sincj)- co s<f> -d<j>. (A-32)

If we let y = costf) , dy = -sin<J)'d<j) and

< =

2

E

I =

2

2 r°

17 ' (t)

' I LI^-(-d ^)> ( A~ 33 )

2 r

1

*• (f)

• I L^-ydy, (A-34)

3 where L (y) for y = 1 and 0.23 are available from Kohl, et al [22], Following Kohl

A et al [23], L (y) is assumed to be a straight line from y = 1 to y = 0.23 and from

A y = 0.23 to y = 0, and L(0) is assumed to be zero. This simple functional dependence

of L (y) is estimated [23] to be accurate to a few percent. With these assumptions

L^(0.23)

L

A (y) = —cT~23—

* y f ° r y =

° t0 °' 23 (A-35)

and

e L*(0.23) -0.23L*(1) (l*(1) -L*(0.23))y

L, (v) = 7T^ +

A XH/ 0.77 0.77

(A-36)

for y = 0.23 to 1.

Substituting this into eq. (A-34) and performing the integrations, we obtain, using

a = 6.96-108 [m] and R = 1.496-1011

[m]

,

Ef = 136-10

_6

-[0.2050.L^(0.23) + 0.2861-L®"(1)1 . (A-37)

A A A

Direct measurements of (spectrally averaged) extraterrestrial solar irradiance are available for a spectral slit width of 1.0 [nm] [24] and 0.34 [nm] [25]. These spece e trally averaged quantities E are related to E by the expression

A A

62
I

E^-z-dA

£ = ^

(A-38)

•dA AA

where z is the slit-scattering function. Computations of E using eqs. (A-37) and

A (A-38) and a triangular slit function (best estimate available) were compared to the direct

measurements. Though the relative spectral values agreed within a few percent, the values

themselves differed by factors of 0.852 (1.0 [nm] slit) and 0.813 (0.34 [nm] slit),

the computed being larger than the observed in each case. We decided to use the more

recent 1.0 [nm] data of Heath so we normalized eq. (A-37) by the factor of 0.852.

That is,

E*: = 0.852.136-10" 6 -[0.2050-L

<T(0.23) + 0. 2861-L

<T(1)] . (A-39)

Tables A-l and A-2 give values of E convoluted (eq. A-38) with a triangular slitA scattering function having a spectral slit width AA of 0.18 [nm] and 1.0 [nm]

,

respectively.

Finally, we have all that is needed to compute the terrestrial solar spectral irradiance E for A < 310 [nm] which are the wavelengths of major interest to us. Figure 3 -1

is the result of this calculation using q =0.5 and S„ = 0.003 [nm ] and Bass'

k„(t ,A). For a spectral slit width AA >> 0.003 [nm] , such as in figures 2 or 4, one must convolute the computed E, with the slit-scattering function of the instrument; that

A is,

/ E -z-dA

Aa Ear = —^

(a-4o)

/ z-dA

-/AA

For figures 2 and 4, triangular slit-scattering functions were used with the spectral

widths indicated in the figures.

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77
References

[1] G. M. B. Dobson, "Observer's Handbook for the Ozone Spectrophotometer", Annals of

the International Geophysical Year, 5^ (Pergamon Press, New York, 1957-1958) 46-81.

[2] L. M. Garrison, L. E. Murray, and A. E. S. Green, "Ultraviolet Limit of Solar

Radiation at the Earth's Surface with a Photon Counting Monochromator",

Appl. Opt., 17> No - 5 (March 1, 1978) 683-684.

[3] L. M. Garrison, D. D. Doda, and A. E. S. Green, "Total Ozone Determination by

Spectroradiometry in the Middle Ultraviolet", Appl. Opt., 18, No. 6 (March 15, 1979)

850-855.

[4] Henry J. Kostkowski and Fred E. Nicodemus, "An Introduction to the Measurement

Equation", Chapter 5 of "Self-Study Manual on Optical Radiation Measurements:

Part I—Concepts", Nat. Bur. Stand. (U.S.), Tech. Note 910-2, 118 pages (Feb. 1978)

pp. 58-92.

[5] Fred E. Nicodemus, "Physically Defining Measurement-Beam Geometry by Using Opaque

Barriers", Chapter 9 of "Self-Study Manual on Optical Radiation Measurements:

Part I—Concepts", Nat. Bur. Stand. (U.S.), Tech. Note 910-4, 134 pages (June 1979)

pp. 91-119.

[6] Henry J. Kostkowski, "The Relative Spectral Responsivity and Slit-Scattering Function

of a Spectroradiometer", Chapter 7 of "Self-Study Manual on Optical Radiation

Measurements: Part I —Concepts", Nat. Bur. Stand. (U.S.), Tech. Note 910-4,

134 pages (June 1979) pp. 2-34.

[7] Paul Bener, "Approximate Values of Intensity of Natural Ultraviolet Radiation for

Different Amounts of Atmospheric Ozone", Physikalisch-Meteorologisches Observatorium

Davos, Davos-Platz, Switzerland, ARDG(E) Contract No. DAJA37-68-C-107 , Final Tech.

Rept., Feb. 71-Feb. 72, (June 1972) [NTIS, AD 752-115].

[8] Henry J. Kostkowski, "Precise Instruments and Accurate Standards Do Not Insure

Accurate Measurements", Optical Radiation News, Radiometric Physics Division,

Nat. Bur. Stand. (U.S.), No. 28 (April 1979).

[9] John B. Shumaker, "Distribution of Optical Radiation with Respect to Polarization",

Chapter 6 of "Self-Study Manual on Optical Radiation Measurements: Part I

Concepts", Nat. Bur. Stand. (U.S.), Tech. Note 910-3, 62 pages (June 1977) pp. 1-53.

[10] L. M. Garrison, Z. Blaszczak, and A. E. S. Green, "Polarization Characteristics of an Altazimuth Sky Scanner", Appl. Optics, 1_9, No. 9, (May 1, 1980) 1419-1424.

[11] John B. Shumaker, "Deconvolution", Chapter 8 of "Self-Study Manual on Optical

Radiation Measurements: Part I —Concepts", Nat. Bur. Stand. (U.S.). Tech. Note

910-4, 134 pages (June 1979) pp. 35-90.

[12] Robley D. Evans, "The Atomic Nucleus", Chapter 28 (McGraw-Hill Book Company,

New York, 1955).

[13] R. D. Saunders and J. B. Shumaker, "Optical Radiation Measurements: The 1973 NBS

Scale of Spectral Irradiance", Nat. Bur. Stand. (U.S.), Tech. Note 594-13,

36 pages (April 1977).

[14] L. M. Garrison, L. E. Murray, D. D. Doda, and A. E. S. Green, "Diffuse-Direct

Ultraviolet Ratios with a Compact Double Monochromator", Appl. Optics, 17 , No. 6, (March 1, 1978) 827-836; also A. T. Chai and A. E. S. Green, "Ratio

Measurement of Diffuse to Direct Solar Irradiances in the Middle Ultraviolet",

Appl. Optics, 15, No. 5 (May 1976) 1182-1187.

78
[15] F. E. Nicodemus and H. J. Kostkowski, "Distribution of Optical Radiation with

Respect to Position and Direction—Radiance", Chapter 2 of "Self-Study Manual

on Optical Radiation Measurements: Part I —Concepts", Nat. Bur. Stand. (U.S.),

Tech. Note 910-1, 93 pages (Mar. 1976) pp. 10-44.

[16] Fred E. Nicodemus, "More on the Distribution of Optical Radiation with respect

to Position and Direction", Chapter 4 of "Self-Study Manual on Optical Radiation

Measurements: Part I —Concepts", Nat. Bur. Stand. (U.S.), Tech. Note 910-2,

118 pages (Feb. 1978) pp. 1-57.

[17] Alex E. S. Green and P. F. Schippnick, "UV-B Reaching the Surface", in "The Role of

Solar Ultraviolet Radiation in Marine Ecosystems", John Calkins, ed. (Plenum Press,

in publication)

.

[18] Arnold M. Bass and Richard J. Paur, National Bureau of Standards, Washington, D.C.,

20234, personal communication.

[19] A. E. S. Green, K. R. Cross and L. A. Smith, "Improved Analytic Characterization

of Ultraviolet Skylight", Photochem. and Photobiol. , 31, No. 1 (Jan. 1980)

pp. 59-65.

[20] United States Committee on Extension to the Standard Atmosphere. U.S. Standard

Atmosphere, 1962. Supplements, 1966. Prepared under sponsorship of Environmental

Science Services Administration, National Aeronautics and Space Administration,

and the United States Air Force. (Superintendent of Documents, U.S. Government

Printing Office, Washington, D.C. 20402; 1966) p. 17.

[21] A. E. S. Green, T. Sawada and E. P. Shettle, "The Middle Ultraviolet Reaching the

Ground", Photochem. and Photobiol., 19, (1974) pp. 251-259.

[22] John L. Kohl, William H. Parkinson and Robert L. Jurucz , "Center and Limb Solar

Spectrum in High Spectral Resolution 225.2 nm to 319.6 nm", Smithsonian Center

for Astrophysics (Harvard University Printing Office, Cambridge, 1978).

[23] John L. Kohl, William H. Parkinson, and Carlos A. Zapata, "Solar Spectral Radiance

and Irradiance, 225.2 nm to 319.6 nm", The Astrophysical Journal Supplement Series,

Vol. 44 (Nov. 1980) pp. 295-317.

[24] D. F. Heath, Goddard Space Flight Center, Greenbelt , Maryland 20771, personal

communication.

[25] A. Lyle Broadfoot, "The Solar Spectrum 2100-3200 A", The Astrophysical Journal,

173 (May 1972) pp. 681-689.

[26] John B. Shumaker, "Introduction to Coherence in Radiometry", Chapter 10 of

"Self-Study Manual on Optical Radiation Measurements; Part I —Concepts",

Nat. Bur. Stand. (U.S.) Tech. Note 910-6 (in preparation).

79
ADDENDUM to Chapter 4 in NBS Tech Note 910-2 :

p. 28; 1st line below eq. (4.35):

Insert a superscript one - - - inverse- square law1 - - - referring to the following footnote at the bottom of the page:

'See Explanatory Note following end of Appendix 4 on p. 102,

p. 102, following end of Appendix 4, add:

Explanatory Note concerning unit-dimensions in eq. (4.36) on p . 28 as an expression of the inverse-square law.

In this Manual we have insisted on the need for recognizing and treating solid

angles as having a unit-dimension of [sr], as in Tables 4-1, 4-2, and 4-3, on pp. 3 to

6, inclusive. However, in eq. (4.36) there appears to be an exception to this where we

take the quotient of I [W«sr ] and the square of D [m] and equate that quotient to _2

dE = dF [W*m ], seemingly ignoring the unit-dimension [sr]. Actually, there is no

inconsistency and the [sr] is not ignored. To demonstrate this, we need to distinguish

between the always orthogonal radial lengths, with dimension [L ] or unit-dimension

[m ], and transverse lengths, with dimension [L ] or unit -dimension [m ]

, as discussed in examining the concepts of plane angle and solid angle and their dimensionality

in Appendix 2 of NBS Tech Note 910-1, particularly on p. 69. In those terms, the unitdimension of a plane angle is [6] = [m *m ] and that of a solid angle is

2 -2

[to] = [m *m ] (the quotient of the dimensions of an intercepted or enclosed area

subtended by the solid angle on the surface of a sphere about its vertex divided by the

dimensions of the square of the radius of that sphere). In eq. (4.36), the unit dimension of D, the distance along the direction of propagation, is clearly [D] = [m ]

not [ml. But that of the normal irradiance dE or fluence rate dF . the flux per

t n t _2

unit area perpendicular to the direction of propagation, is [dE ] = [dF ] = [W*m ] _2

not [W*m ] . The unit dimensions of radiant intensity I are then

—1 —2 2 2 [I] = [W«sr ] = [W*m *m ]. Accordingly, the unit dimensions of the quotient I/D

-2 -2 2 -2 -2 are [I'D ] = [W*m *m *m ] = [W*m ] = [dF ] = [dE ], so we are consistent after

all.

80
NBS-114A (REV. 2-8C) U.S. DEPT. OF COMM. BIBLIOGRAPHIC DATA

SHEET (See instructions)

1, -PUBLICATION OR

REPORT NO.

NBS TN 910-5

2. Performing Organ. Report No. 3. Publication Date

December 1982

4. TITLE AND SUBTITLE

SELF-STUDY MANUAL ON OPTICAL RADIATION MEASUREMENTS, Part Ill—Applications

Chapter 1. Measurement of Solar Terrestrial Spectral Irradiance in the

Ozone Cut-Off Region

5. AUTHOR(S) Henry J. Kostkowski, Robert D. Saunders, John F. Ward,

Charles H. Popenoe, and A.E.S. Green

6. PERFORMING ORGANIZATION (If joint or other than NBS. see instructions)

NATIONAL BUREAU OF STANDARDS

DEPARTMENT OF COMMERCE

WASHINGTON, D.C. 20234

7. Contract/Grant No.

8. Type of Report & Period Covered

Final

9. SPONSORING ORGANIZATION NAME AND COMPLETE ADDRESS (Street. City. State. ZIP)

Same as Item 6.

10. SUPPLEMENTARY NOTES

~\ Document describes a computer program; SF-185, FIPS Software Summary, is attached.

11. ABSTRACT (A 200-word or less factual summary of most significant information. If document includes a significant

bibliography or literature survey, mention it here)

This is the first chapter in Part III (Applications) of this Manual.

Material developed in earlier chapters is used to perform state-of-the-art

measurements in Gainesville, Florida, of solar terrestrial spectral irradiance

between 290 [nm] and 340 [nm] . The measurement equation is used to design the

experiment and to address the effects of polarization, non-linearity, spectral

scattering, distortion, slit-scattering function, spectral irradiance calibration, and wavelength calibration. Estimates are made of the uncertainties

associated with all these factors. The total uncertainty is estimated to be

about 10 percent. An appendix includes details for computing the solar terrestrial spectral irradiance between 280 and 310 [nm] . Suggestions are made for

reducing the uncertainty by about one third and for further research in UV

solar terrestrial measurements.

12. KEY WORDS (Six to twelve entries; alphabetical order; capitalize only proper names; and separate key words by semicolons)

atmospheric attenuation; atmospheric ozone; optical radiation measurements;

radiometry; solar radiation; spectroradiometry; UV spectral measurements.

13. AVAILABILITY

fXI Unlimited

| | For Official Distribution. Do Not Release to NTIS

fXl Order From Superintendent of Documents, U.S. Government Printing Office, Washington, D.C.

20402. Q Order From National Technical Information Service (NTIS), Springfield, VA. 22161

14. NO. OF

PRINTED PAGES

91

15. Price

$5.50

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Technical Notes—Studies or reports which are complete in themselves but restrictive in their treatment of a subject. Analogous to monographs but not so comprehensive in scope or definitive in treatment of the subject area. Often serve as a vehicle for final reports of work performed at NBS under the sponsorship of other government agencies.

Voluntary Product Standards—Developed under procedures

published by the Department of Commerce in Part 10, Title 15, of

the Code of Federal Regulations. The standards establish nationally recognized requirements for products, and provide all concerned interests with a basis for common understanding of the

characteristics of the products. NBS administers this program as a supplement to the activities of the private sector standardizing

organizations. Consumer Information Series—Practical information, based on N BS research and experience, covering areas of interest to the con- sumer. Easily understandable language and illustrations provide

useful background knowledge for shopping in today's tech- nological marketplace. Order the above NBS publications from: Superintendent of Documents, Government Printing Office. Washington. DC 20402. Order the following NBS publications—FIPS and NBSlR's—from

the National Technical Information Service . Springfield. VA 22161

.

Federal Information Processing Standards Publications (FIPS

PUB)—Publications in this series collectively constitute the Federal Information Processing Standards Register. The Register

serves as the official source of information in the Federal Govern- ment regarding standards issued by NBS pursuant to the Federal Property and Administrative Services Act of 1949 as amended,

Public Law 89-306 (79 Stat. 1127), and as implemented by Executive Order 1 1717 (38 FR 12315, dated May 1 1, 1973) and Part 6

of Title 15 CFR (Code of Federal Regulations).

NBS Interagency Reports (NBSIR)—A special series of interim or

final reports on work performed by NBS for outside sponsors

(both government and non-government). In general, initial dis- tribution is handled by the sponsor; public distribution is by the National Technical Information Service , Springfield, VA 22161,

in paper copy or microfiche form.
U.S. Department of Commerce

National Bureau of Standards

Washington, DC. 20234

Official Business

Penalty for Private Use $300

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