- j 

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* MS-i-66-02 

October, 1966 

V/LL€, ALABAMA 

FY 1966 SCIENTIFIC AND TECHNICAL REPORTS 

ARTICLES, PAPERS, AND PRESENTATIONS 

Management Services Office (, I 

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CFSTl PRICE(S) $ :: 

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1 MSFC - Form 454 (Revised September 1961) -* 
. 

ABSTRACT 

This document presents the formal NASA technical reports, the papers published in technical journals, 

and the presentations made by MSFC personnel in FY 66. Also included are the papers and presentations of 

MSFC Contractors. It does not include internal information documents. 

It is prepared according to subject category using the NASA subject category list. 

All of the NASA series reports herein may be obtained from the Scientific and Technical Information 

Facility after being announced in STAR or C STAR. 

The information in this report will be of invaluable assistance to the scientific and engineering community in helping them to determine what has been published and how they can obtain information on the 

subjects covered. 

I' 
MS-1-66-02 October, 1966 

FY 1966 SCIENTIFIC AND TECHNICAL REPORTS 

ARTICLES, PAPERS, AND PRESENTATIONS 

Scientific and Technical Information Branch 

Management Services Office 
FOREWORD 

In accordance with the NASA Space Act of 1958 the MSFC has provided for the widest practicable and 

appropriate dissemination of information concerning its activities and the results thereof. 

Records kept over the years indicate that the technical information output of MSFC has increased in 

keeping with the increased missions of the Center. 

Since July I, 1960, when the George C. Marshall Space Flight Center was organized, the reporting 

of scientific and engineering information has been considered a prime responsibility of the Center. Our credo 

has been that "research and development work is valuable, but only if its results can be communicated and 

made understandable to others". 
GEORGE C. MARSHALL SPACE FLIGHT CENTER 

Huntsville, Alabama 

~y 1966 SCIENTIFIC AND TECHNICAL REPORTS, ARTICLES, PAPERS, AND PRESENTATIONS 

TABLE OF CONTENTS 

Page 

01. AERODYNAMICS ................................................... 1 

06. CHEMISTRY ....................................................... 2 

07. COMMUNICATIONS ................................................. 2 

10. ELECTRONICS 2 

12. FLUIDMECHANICS ................................................. 

.................................................... 

3 

13. GEOPHYSICS 4 

14. INSTRUMENTATIONANDPHOTOGRAPHY .................................. 

15. MACHINE ELEMENTS AND PROCESSES ................................... 

17. MATERIALS, METALLIC.. ............................................ 

..................................................... 

4 

5 

5 

18. MATERIALS, NONMETALLIC .......................................... 8 

19. MATHEMATICS .................................................... 8 

20. METEOROLOGY ................................................... 8 

21. NAVIGATION ..................................................... 8 

23. PHYSICS, GENERAL ................................................. 9 

27. PROPELLANTS .................................................... 9 

28. PROPULSIONSYSTEMS ............................................... 9 

29. SPACE RADIATION .................................................. 9 

30. SPACESCIENCES ................................................... 10 

31. SPACEVEHICLES .................................................. 12 

32. STRUCTURALMECHANICS ............................................ 14 

33. THERMODYNAMICS AND COMBUSTION ................................... 15 

34. GENERAL ........................................................ 1G 

Contractor Reports .................................................. 17 

Articles, Papers ,and Presentations, by MSFC Personnel .......................... 83 

* Before title indicates classified document. 
NASA TM X-53307 July 26, 1965 NASA TM X-53401 February 24, 1966 

STATIC AERODYNAMIC CHARACTERISTICS OF THE 

APOLLO - SATURN V VEHICLE 

RANGE SAFETY AERODYNAMIC CHARACTERISTICS 

OF THE APOLLO-SATURN IB VEHICLES 

Victor K. Henson, Aero-Astrodynamics Laboratory. Billy W. Nunley , Aero-Astrodynamics Laboratory. 

NASA TM X-53336 September 28, 1965 NASA TM X-53410 March 14, 1966 

PHOTOGRAMMETRIC DATA EDITING, PROCESSING 

AND ANALYSIS TECHNIQUES FOR A SMOKE TRAIL 

WIND PROFILE MEASUREMENT PROGRAM 

STUDY OF POROUS WALL LOW DENSITY WIND 

TUNNEL DIFFUSERS 

K. W. Rogers, A. T. LindsayandM. R. Bottorff, 

Bobby G. Junkin, Computation Laboratory. Aero-Astrodynamics Laboratory. 

NASA TM X-53348 October 12, 1965 NASA TM X-53414 March 22, 1966 

STATIC AERODYNAMIC CHARACTERISTICS OF THE 

APOLLO-SATURN IB VEHICLE 

GENERAL FORMULATION OF THE ITERATIVE 

GUIDANCE MODE 

Billy W. Nunley , Aero-Astrodynamics Laboratory. I. E. Smith, Aero-Astrodynamics Laboratory. 

NASA TM X-53363 December 3, 1965 NASA TM X-53423 March 30, 1966 

MEASUREMENTS OF WINDS BY CHEMICAL 

RELEASES IN THE UPPER - ATMOSPHERE 

STATIC AERODYNAMIC CHARACTERISTICS OF THE 

ABORTED APOLLO-SATURN IB VEHICLE 

Hugh Wilson Morgan, Aero-Astrodynamics Laboratory. Billy W. Nunley , Aero-Astrodynamics Laboratory. 

NASA TM X-53365 December 3, 1965 NASA TM X-53473 June 7, 1966 

A WORST DISTURBANCE DESIGN CRITERION IN 

THE THEORY OF ANALYTICAL CONTROL SYSTEMS 

SYNTHESIS 

BOUNDARY VALUE PROBLEMS ASSOCIATED WITH 

OPTIMIZATION THEORY 

Hugo L. Ingram, Aero-Astrodynamics Laboratory. 

Thomas E. Carter, Aero-Astrodynamics Laboratory. 

NASA TM X-53389 October 15, 1965 

AERO-ASTRODYNAMICS RESEARCH REVIEW NO. 3. 

Aero-Astrodynamics Laboratory. 

NASA TN D-3088 December, 1965 

AERODYNAMIC CHARACTERISTICS OF SPHERICALLY 

BLUNTED CONES AT MACH NUMBERS FROM 0.5 

TO 5.0 

NASA TM X-53391 February 7, 1966 Robert V. Owens, Aero-Astrodynamics Laboratory. 

NEWTONIAN AERODYNAMICS FOR GENERAL BODY 

SHAPES WITH SEVERAL APPLICATIONS 

W. H. Heybey, Aero-Astrodynamics Laboratory. 

1 
AERODYNAMICS (Concluded) 

NASA TN D-3117 November, 1965 NASA TN D-3125 January, 1966 

MONTECARLOAPPROACHTOTOUCHDOWN ANEWAPPROACHTOTHEEXPLANATIONOFTHE 

DYNAMICS FOR SOFT LUNAR LANDING FLUTTER MECHANISM 

Robert E. Lavender, Aero-Astrodynamics Laboratory. Mario H. Reinfurth and Fredrick W. Swift, AeroAstrodynamics Laboratory. 

, 06 CHEMISTRY 

NASA TM X-53383 1965 

RESEARCH ACHIEVEMENTS REVIEW SERIES NO. 7 

W. R. Lucas, Propulsion and Vehicle Engineering 

Laboratory. 

07 COMMUNICATIONS 

NASA TM X-53321 August 17, 1965 NASA TN D-3405 May, 1966 

SPACE VEHICLE SA-7 TELEMETRY SYSTEM 

Telemetry Performance Evaluation Office, Astrionics 

Laboratory. 

INFORMATION TRANSFER SYSTEMS IN SPACE 

COMMUNICATIONS 

Amadeo Dabul, Quality and Reliability Assurance 

Laboratory. 

NASA TM X-53350 October 22, 1965 

SATURN INSTRUMENT UNIT COMMAND SYSTEM 

H. R. Lowery, Astrionics Laboratory. 

10 ELECTRONICS 

NASA TM X-53364 July, 1965 

RESEARCH ACHIEVEMENTS REVIEW SERIES NO. 5 

"ELECTRONICS" 

Joseph L. Randall, James C. Taylor, and Charles 

L. Wyman, Aero-Astrodynamics Laboratory. 

NASA TM X-53384 February 1, 1966 

THE ASTRIONICS SYSTEM OF SATURN LAUNCH 

VEHICLES 

* NASA TM X-53398 February 23, 1966 

SATURN I BLOCK I1 GUIDANCE SUMMARY REPORT 

R. A. Chapman, Aero-Astrodynamics Laboratory. 

NASA TM X-53435 April 12, 1966 

INVESTIGATION OF THE DEFLECTION OF AN 

ELECTRON BEAM AS A MEANS OF MEASURING 

ELECTRIC FIELD STRENGTH 

E. L. Shriver, Research Projects Laboratory. 

Rudolf Decher, Astrionics Laboratory. 

NASA TM X-53394 1965 

RESEARCH ACHIEVEMENTS REVIEW SERIES NO. 13 

NASA TN D-2948 August, 1965 

ANALYTICAL DETERMINATION OF TRANSFER 

FUNCTIONS FOR RC COMMUTATED NETWORKS 

Astrionics Laboratory. 

2 

S. N. Carroll, Astrionics Laboratory. 
12 FLUID MECHANICS 

NASA TM X-53269 August 4, 1965 NASA TM X-53386 February 1, 1966 

CALCULATIONS OF MASS-FLOW AND THRUST 

PRODUCED FOR A TWO-PHASE FLUID MIXTURE 

PASSING THROUGH A CHOKED NOZZLE 

A MONTE CARLO PROGRAM FOR TRANSMISSION 

PROBABILITY CALCULATIONS INCLUDING MASS 

MOTIONS I' 

1. Wyley D. Ward, (Brown Engineering Company, Inc.) 

Propulsion and Vehicle Engineering Laboratory. 

James 0. Ballance, Aero-Astrodynamics Laboratory. 

NASA TM X-53395 February 10, 1966 

NASA TM X-53330 August 18, 1965 

FLUID QUALITY IN A SELF-PRESSURIZED CONTAINER DISCHARGE LINE 

PROGRAM PLAN FOR EARTH-ORBITAL LOW G 

HEAT TRANSFER AND FLUID MECHANICS 

EXPERIMENTS 

Hugh M. Campbell, Jr. , Propulsion and Vehicle 

Engineering Laboratory. 

M. E. Nein and C. D. Arnett, Propulsion and 

Vehicle Engineering Laboratory. 

NASA TM X-53341 October 5, 1965 NASA TM X-53402 March 1, 1966 

VIBRATION AND ACOUSTIC ANALYSIS SATURN 

SA-8 FLIGHT 

SPACE THERMAL CONTROL USING PHASE CHANGE 

Tommy C. Bannister, Research Projects Laboratory. 

Measuring and Evaluation Section, Propulsion and 

Vehicle Engineering Laboratory. 

NASA TM X-53411 March 15. 1966 

NASA TM X-53344 October 7. 1965 USE OF THE CURTIS-GODSON APPROXIMATION 

IN CALCULATIONS OF RADIANT HEATING BY 

GROUND LEVEL ACOUSTICAL FOCI IN A THREE- INHOMOGENEOUS HOT GASES 

LAYERED ATMOSPHERE 

B. Krakow, H. J. Babrov, G. J. Maclay, and A. L. 

Willi H. Heybey, Aero-Astrodynamics Laboratory. Shabott, Aero-Astrodynamics Laboratory. 

NASA TM X-53353 September 17, 1965 NASA TM X-53454 April 27, 1966 

PRESSURE DISTRIBUTION AND BUBBLE FORMATION INDUCED BY LONGJTUDINAL VIBRATION OF 

A FLEXIBLE LIQUID-FILLED CYLINDER 

A NEW CONCEPT TO THE GENERAL UNDERSTANDING OF THE EFFECTS OF LONGITUDINAL CONDUCTION FOR MULTISTREAM COUNTERFLOW HEAT 

EXCHANGERS 

R. J. Schoenhals and T. J. Overcamp, Propulsion 

and Vehicle Engineering Laboratory. C. L. Pan, N. E. Welch, R. R. Head, Propulsion 

and Vehicle Engineering Laboratory. 

NASA TM X-53368 December 13, 1965 

NASA TN D-3089 January, 1966 

NUMERICAL PROCEDURE FOR ROLL STABILITY 

STUDIES THE GENERAL INSTABILITY OF RING-STIFFENED 

CORRUGATED CYLINDERS UNDER AXIAL COM- 

.Philip J. Hays, Aero-Astrodynamics Laboratory. PRESSION. 

John N. Dickson and Richard H. Brolliar,( Brown 

Engineering Co.), Propulsion and Vehicle Engineering 

Laboratory. 

3 
FLUID MECHANICS (Concluded) 

NASA TN D-3156 December, 1965 NASA TN D-3178 January, 1966 

PRESSURE FLUCTUATIONS IN TURBULENT BOUN- INTERACTION OF STRUCTURE AND LIQUID IN THE 

DARY LAYERS SOUND SUPPRESSOR SYSTEM 

M. V. Lowson, (Wylie Laboratories), Aero-Astrodynamics Laboratory. Technology, Test Laboratory. 

Helmut F. Bauer, Consultant, Georgia Institute of 

NASA TN D-3398 May, 1966 

PREDICTED ACOUSTICAL PERFORMANCE OF THE 

S-IC SOUND SUPPRESSOR 

NASA TN D-3165 January, 1966 

LIQUID BEHAVIOR IN THE RESERVOIR OF THE 

SOUND SUPPRESSOR SYSTEM 

Helmut F. Bauer, Consultant, Georgia Institute of 

Technology, Test Laboratory. 

Fritz Kramer, Test Laboratory. 

NASA TN D-3440 June, 1966 

NASA TN D-3176 December, 1965 

LIQUID CAVITATION STUDIES IN CIRCULAR PIPE 

BENDS SUPERSONIC FLOW 

QUASI-SLENDER BODY THEORY FOR SLOWLY 

OSCILLATING BODIES OF REVOLUTION IN 

R. E. Stonemetz, Propulsion and Vehicle Engineering 

Laboratory. dynamics Laboratory. 

Max F. Platzer and Gilbert H. Hoffman, Aero-AstroI 

13 GEOPHYSICS 

NASA TM X-53303 July 26, 1965 

HOPI-DART AND CAJUN-DART ROCKET WIND 

MEASURING SYSTEMS 

Robert E. Turner and Luke P. Gilchrist, Aero-Astrodynamics Laboratory. 

14 INSTRUMENTATION AND PHOTOGRAPHY 

NASA TN D-3003 October, 1965 

PRELIMINARY CONSIDERATIONS OF OPTICAL 

TELESCOPES FOR LUNAR SURFACE USE 

Ernest H. Wells, Research Projects Laboratory, 

NASA TM X-53416 March 24, 1966 

EVALUATION OF AN AUTOMATIC AEROSOL 

PARTICLE COUNTER FOR MEASURING THE 

AIRBORNE CONTAMINATION LEVEL IN A CONTROLLED ENVIRONMENT 

Theodore W. Lewis, Manufacturing Engineering 

Laboratory. 

4 
15 MACHINE ELEMENTS AND PROCESSES 

NASA TM X-53312 

MACHINING AND GRINDING OF TITANIUM AND ITS 

ALLOYS 

August 4, 1965 

C. T. Olofson, F. W. Boulger, J. A. Gurklis 

Prepared under the Supervision of the RSIC, Directcrate of Rssearch and Development, U. S. Army 

Missile Command,Redstone Arsenal, Alabama. 

NASA TM X-53335 October 15, 1965 

THE EFFECTS OF GOLD PLATING ON SOLDERED 

CONNECTIONS 

S. D. Ebneter, Quality and Reliability Assurance 

Laboratory. 

NASA TM X-53430 October, 1965 

THE MAKING OF NICKEL AND NICKEL ALLOY 

SHAPES BY CASTING, POWDER METALLURGY, 

TION AND METAL SPRAYING (continued) 

ELECTROFORMING, CHEMICAL VAPOR DEPOSI17 MATERIALS, 

NASA TM X-53302 July 23, 1965 

LOW TEMPERATURE MECHANICAL PROPERTIES 

OF HP 9-4-25 ALLOY 

W. R. Morgan, Pmpulsion and Vehicle Engineering 

Laboratory. 

NASA TM X-53313 

ADHESIVE BONDING OF TlTANIUM AND ITS ALLOYS 

August 4, 1965 

R. E. Keith, R. E. Monroe, D. C. Martin 

Prepared under the Supervision of the RSIC, Directorate of Research and Development, U. S. Army Missile 

Command, Redstone Arsenal, Alabama. 

NASA TM X-53317 August 9, 1965 

STRESS CORROSION STUDIES OF AM - 355 STAINLESS STEEL 

J. G. Williamson, Propulsion and Vehicle Engineering 

Laboratory . 

J. G. Kura, V. D. Barth, W. H. Safranek, E. T. 

Hall, H. McCurdy, and H. 0. McIntire, Prepared 

under the supervision of the Research Branch, RSIC, 

Directorate of Research and Development, U. S. 

Army Missile Command, Redstone Arsenal, Alabama. 

NASA TM X-53432 October, 1965 

WELDING PROCEDURES FOR TITANIUM AND 

TITANIUM ALLOYS 

J. J. Vagi, R. E. Monroe, R. M. Evans, and D. C. 

Martin, Prepared under the supervision of the 

Research Branch,RSIC, Directorate of Research and 

Development, U. S. Army Missile Command, 

Redstone Arsenal, Alabama. 

NASA TN D-3452 May, 1966 

SETS OF SIMILARITY RATIOS FOR THERMAL 

MODELING 

J. R. Watkins, Research Projects Laboratory, 

METALLIC 

NASA TM X-53329 September 13, 1965 

EXPERIMENTAL X-RAY STRESS ANALYSIS FOR 

PRECIPITATION HARDENED ALUMINUM ALLOYS 

James H. Wharton and William L. Prince, Propulsion 

and Vehicle Engineering Laboratory. 

NASA TM X-53332 September 14, 1965 

LOW TEMPERATURE MECHANICAL PROPERTIES 

OF ALUMINUM ALLOY 2219 - T87, 0.040-INCH 

THICK SHEET THROUGH 5.000-INCH THICK PLATE 

C. R. Denaburg, Propulsion and Vehicle Engineering 

Laboratory. 

NASA TM X-53378 January 13, 1966 

1965 PUBLICATIONS 

Materials Division, Propulsion and Vehicle 

Engineering Laboratory. 

5 
MATERIALS, METALLIC (Continued) 

NASA TM X-53390 February 9, 1966 

STATUS REPORT: DEVELOPMENT OF POLYMERIC 

MATERIALS FOR POTTING AND ENCAPSULATING 

ELECTRONIC ASSEMBLIES 

William J. Patterson, propulsion and Vehicle 

Enginebring Laboratory. 

NASA TM X-53404 March 2, 1966 

GALVANIC CORROSION OF ALUMINUM ASSEMBLIES 

BY STAINLESS STEEL WIRE INSERTS 

T. S. Humphries and E. E. Nelson, Propulsion and 

Vehicle Engineering Laboratory. 

NASA TM X-53407 March 9, 1966 

LOW TEMPERATURE MECHANICAL PROPERTIES 

OF HIGH STRENGTH A-286 BOLTS 

J. W. Montano, Propulsion and Vehicle Engineering 

Laboratory. 

NASA TM X-53427 April 12, 1966 

A CALCULATION METHOD FOR THE ABLATION 

OF GLASS-TIPPED BLUNT BODIES 

John D. Warmbrod, Aero-Astrodynamics Laboratory. 

NASA TM X-53428 October, 1965 

ADHESIVE BONDING OF NICKEL AND NICKELBASE ALLOYS 

R. E. Keith, R. E. Monroe, andD. C. Martin, 

Prepared under the supervision of the Research 

Branch, RSIC, Directorate of Research and Development, U. s. Army Missile Command, Redstone 

Arsenal, Alabama. 

NASA TM X-53429 October, 1965 

SURFACE TREATMENTS FOR TITANIUM ALLOYS 

Manley W. Mallett, Prepared under the supervision 

of the Research Branch, RSIC, Directorate of 

Research and Development, U. S. Arniy Missile 

Command, Rctlstone Arsenal, AIahm:l. 

NASA TM X-53431 October, 1965 

DEFORMATION PROCESSING OF PRECIPITATIONHARDENABLE STAINLESS STEELS 

D. E. Strohecker, A. F. Gerds, andF. W. Boulger, 

prepared under the supervision of the Research Branch, 

RSIC, Directorate of Research and Development, 

U. S. Army Missile Command, Redstone Arsenal, 

Alabama. 

NASA TM X-53433 October, 1965 

MACHINING AND GRINDING OF ULTRAHIGHSTRENGTH STEELS AND STAINLESS STEEL ALLOYS 

C. T. Olofson, J. A. Gurklis, and F. W. Boulger, 

prepared under the supervision of RSIC, Directorate 

of Research and Development, U. S. Army Missile 

Command, Redstone Arsenal, Alabama. 

NASA TM X-53436 April 18, 1966 

LOW TEMPERATURE THERMAL EXPANSION OF 

STRUCTURAL M ETA Ls 

J. C. Horton, C. F. Smith, and R. C. Ruff, Propulsion and Vehicle Engineering Laboratory. 

NASA TM X-53437 April 18, 1966 

THE MAKING OF TITANIUM AND TITANIUM-ALLOY 

SHAPES BY CASTING, POWDER METALLURGY, 

AND OTHER PROCESSES 

J. G. Kura, V. D. Barth, H. McCurdy, W. H. 

Safranek, E. T. Hall, and H. 0. McIntire, prepared 

under the supervision of the RSIC, Directorate of 

Research and Development, U. S. Army Missile 

Command, Redstone Arsenal, Alabama. 

NASA TM X-53438 April 18, ISGG 

DEFORMATION PROCESSING OF TITANIUlI AND 

ITS ALLOYS 

A. F. Gerds, D. E. Strohecker, T. G. Byrer, and 

F. W. Boulger, prepared under supervision of IISIC. 

Directorate of Research and Developnlcnt, U. S . Army Missile Command, Redstone Arsenal, ,~!l:iI)anu. 
MATERIAIS, METALLIC (Concluded) 

NASA TM X-53439 April 18, 1966 

DEFORMATION PROCESSING OF NICKLE-BASE 

AND COBALT-BASE ALLOYS 

D. E. Strohecker, T. G. Byrer, A. F. Gerds, 

J. H. Gehrke, and F. W. Boulger, prepared under 

the supervision of RSIC, Directorate of Research 

and Development, U. S. Army Missile Command 

Redstone Arsenal, Alabama. 

NASA TM X-53445 April 20, 1966 

HEAT TREATMENT OF TITANIUM AND TITANIUM 

ALLOYS 

F. F. Schmidt and R. A. Wood, prepared under the 

supervision of the Research Branch, RSIC, Directorate of Research and Development, U. S. Army 

Missile Command, Redstone Arsenal, Alabama. 

NASA TM X-53446 April 20, 1966 

NASA TM X-53441 April 20, 1966 

MECHANICAL FASTENING OF NICKEL-BASE ALLOYS 

D. L. Cheever, R. E. Monroe, andD. C. Martin, 

prepared under the supervision of the Research 

Branch, RSIC, Directorate of Research and Development, U. S. Army Missile Command, Redstone 

Arsenal, Alabama. 

NASA TM X-53442 April 20, 1966 

MECHANICAL FASTENING OF TITANIUM AND ITS 

ALLOYS 

D. L. Cheever, R. E. Keith, R. E. Monroe, and 

D. C. Martin, prepared under the supervision of 

the Research Branch, RSIC, Directorate of Research 

and Development, U. S. Army Missile Command, 

Redstone Arsenal, Alabama. 

NASA TM X-53443 April 20, 1966 

THERMAL AND MECHANICAL TREATMENTS FOR 

NICKEL AND SELECTED NICKEL-BASE ALLOYS 

AND THEIR EFFECT ON MECHANICAL PROPERTIES 

C. J. Slunder and A. M. Hall, prepared under the 

supervision of the Research Branch, RSIC, Directorate 

of Research and Development, U. S. Army Missile 

Command, Redstone, Alabama. 

NASA TM X-53444 April 20, 1966 

THE CASTING AND POWDER-METALLURGY 

FORMING OF PRECIPITATION-HARDENABLE 

STAINLESS STEELS 

MACHINING AND GRINDING OF NICKEL- AND 

COBALT-BASE ALLOYS 

C. T. Olofson, J. A. Gurklis, and F. W. Boulger, 

prepared under the supervision of the Research Branch, 

RSIC, Directorate of Research and Development, 

U. S. Army Missile Command, Redstone, Alabama. 

NASA TM X-53447 April 20, 1966 

JOINING OF NICKEL AND NICKEL-BASE ALLOYS 

J. J. Vagi, R. E. Monroe, R. M. Evans, andD. C. 

Martin, prepared under supervision of the Research 

Branch, RSIC, Directorate of Research and Development, U. S. Army Missile Command, Redstone 

Arsenal, Alabama. 

NASA TM X-53448 April 20, 1966 

SURFACE TREATMENTS FOR NICKEL AND NICKELBASE ALLOYS 

C. M. Jackson and A. M. Hall, prepared under the 

supervision of the Research Branch, RSIC, Directorate 

of Research and Development, U. S. Missile Command. 

Redstone Arsenal,. Alabama. 

J. G. Kura, V. D. Barth, andH. 0. McIntire, 

prepared under supervision of the Research Branch, 

RSIC, Directorate of Research and Development, 

U. S. Army Missile Command, Redstone, Alabama. 

7 
18 MATERIALS, NONMETALIC 

NASA TM X-53331 September 14, 1965 NASA TM X-53358 November 4, 1965 

INVESTIGATION OF THE COEFFICIENT OF 

FRICTION OF VARIOUS GREASES AND DRY FILM 

LUBRICANTS AT ULTRA HIGH LOADS FOR THE 

SATURN HOLD-DOWN ARMS 

K. E. Demorest and A. F. Whitaker, Propulsion 

and Vehicle Engineering Laboratory. 

STATUS REPORT ON CHEMICAL SYNTHESIS OF 

MONOMERIC SELF-SEALANT TYPE ESTERS 

Lawrence R. Moffett, Jr., Propulsion and Vehicle 

Engineering Laboratory. 

19 MATHEMATICS I 

NASA TM X-53420 1966 NASA TN D-2946 August, 1965 

RESEARCH ACHIEVEMENTS REVIEW SERIES No. 20 

"MATHEMATICS AND COMPUTATION" 

ON THE EFFICIENT USE OF PREDICTOR-CORRECTOR 

METHODS IN THE NUMERICAL SOLUTION OF 

DIFFERENTIAL EQUATIONS 

C. L. Bradshaw, Erwin Fehlberg, and Richard F. 

Arenstmf, Computation Laboratory. David Wdabaugh, Assistant Professor and James R 

Wesson, Associate Professor of Mathematics, 

NASA TN D-2920 

Vanderbilt University, Research and Development 

Applications Division, Computation Laboratory. september, 1965 

HIGHER ORDER APPROXIMATION OF RUNGE-KUTTA 

TYPE 

E. Baylis Shanks, Professor of Mamematics at 

Vanderbilt University, Computation Laboratory. 

20 METEOROLOGY 

NASA TM X-53451 April 26, 1966 

PRELIMINARY RESULTS OF ANEMOMETER 

COMPARISON TESTS 

Dennis W. Camp, Aero-Astrodynamics Laboratory. 

2 1 NAVIGATION 

NASA TM X-53352 October 25, 1965 NASA TN D-2983 September, 1965 

SPACE VEHICLE SA-9 TELEMETRY SYSTEM 

Telemetry Performance Evaluation Office, R-ASTRITP, Astrionics Laboratory. 

A GENERAL DESCRIPTION OF THE ST 124-M 

INERTIAL PLATFORM SYSTEM 

Herman E. Thomason, Astrionics Laboratory. 

NASA TN D-2869 July, 1965 

AN ITERATIVE GUIDANCE SCHEME AND ITS 

I APPLICATION TO LUNAR LANDING 

Helmut J. Horn, Daniel T. Martin, and Doris C. 

Chandler, Aero-Astrodynamics Laboratory. 
23 PHYSICS, GENERAL ~ 

v 

NASA April 20, 1966 NASA TN D-3177 TM X-53449 February, 1966 

EXTRATERRESTRIAL APPLICATION OF X-RAY 

DIFFRACTION CRYOGENIC PROPELLANT TANK PRESSURANT 

H. K. Herglotz, E. 1. duPont de Nemours and Co., 

Scientific Payloads Office, Research Projects Laboratory. Vehicle Engineering Laboratory. 

EXPERIMENTAL AND ANALYTICAL STUDIES OF 

REQUIREMENTS 

M. E. Nein and J. F. Thompson, Propulsion and 

27 PROPELLANTS 

NASA 'I'M X-53356 November 3, 1965 

EFFECTS OF VARIOUS ADDITIVES ON PHYSICAL 

PROPERTIES AND PERFORMANCE OF MONOMETHYLHYDRAZINE 

Harold Perkins, Propulsion and Vehicle Engineering 

Laboratory. 

28 PROPULSION SYSTEMS 

NASA TM X-53294 July 13, 1965 NASA TM X-53379 January 20, 1966 

METHODS OF COMPUTING THE TRANSFORMATION 

MATRIX ASSOCIATED WITH GIMBALLESS INERTIAL 

MEASUREMENT UNITS 

Dexter H. Burdeshaw , .4strionics Laboratory. 

SIMULATION OF THE 5-2 ENGINE GIMBAL BEARING 

K. E. Demorest and K. W. Wilks, Propulsion and 

Vehicle Engineering Laboratory. 

NASA TM X-53400 February 24, 1966 

NASA TM X-53334 August 27, 1965 

QUALIFICATIONS OF THE GEMINI SE-7 ENGINE AS 

CALCULATION OF ROCKET PERFORMANCE THE SATURN S-IV B STAGE ULLAGE CONTROL 

PARAMETERS BASED ON THE EQUILIBRIUM 

COMPOSITION OF THE COMBUSTION PRODUCTS 

Klaus W. Gross, Propulsion and Vehicle Engineering 

Laboratory. 

THRUSTER 

Donald E. Pryor, Propulsion and Vehicle Engineering 

Laboratory. 

29 SPACE RADIATION 

NASA TM X-53301 July 1, 1965 NASA TM X-53370 1965 

RADIATION PHYSICS RESEARCH AT MSFC 

Russell D. Shelton, Research Projects Laboratory. 

RESEARCH ACHIEVEMENTS REVIEW SERIES NO. 1 

"RADIATION PHYSICS" 

Russell D. Shelton, Research Projects Laboratory. 

9 
30 SPACE SCIENCES 

NASA TM X-53292 July 12, 1965 NASA TM X-53325 September 2, 1965 

PROGRESS REPORT NO. 7 

ON STUDIES IN THE FIELDS OF SPACE FLIGHT 

AND GUIDANCE THEORY 

STATISTICAL ANALYSE OF PHOTOGRAPHIC 

METEOR DATA - PART I - OPIK'S LUMINOUS 

EFFICIENCY AND SUPPLEMENTED WHIPPLE 

WEIGHTING 

Sponsored by Aero-Astrodynamics Laboratory. 

Charles C. Dalton, Aero-Astrodynamics Laboratory. 

NASA TM X-53297 July 20. 1965 

NASA TM X-53327 September 7, 1965 

MANNED MARS AND VENUS EXPLORATION STUDY 

EXECUTIVE SUMMARY REPORT DERIVATION OF PARAMETRIC VALUES FOR A 

GREENHOUSE MODEL OF THE CYTHEREAN 

J. N. Smith, Advanced Systems Office. ATMOSPHERE I 

Robert B. Owen, Aero-Astrodynamics Laboratory. 

':' NASA TM X-53304 July 26, 1965 

SA 202 LAUNCH VEHICLE REFERENCE TRAJECTORY 

NASA TM X-53340 September 30, 1965 

SATURN SA-IO/ PEGASUS C POSTFLIGHT TRAJECJoseph W. Cremin, William M. Gillis and Thomas TORY 

W. Telfer, Aero-Astrodynamics Laboratory. 

Jonathan B. Haussler and Robert H. Benson, AeroAstrodynamics Laboratory. 

NASA TM X-53309 August 2, 1965 

SATURN SA-8/ PEGASUS B POSTFLIGHT TRAJECTORY 

NASA TM X-53347 October 12, 1965 

EXECUTIVE SUMMARY REPORT 

MISSION REQUIREMENTS FOR MANNED MARS AND 

VENUS EXPLORATION 

Jonathan B. Haussler and Robert H. Benson, 

Aero-Astrodynamics Laboratory. 

J. N. Smith, Advanced Systems Office. 

NASA TM X-53318 August 13, 1965 

EARTH ORBITAL LAUNCH WINDOWS FOR MARS 

MISSIONS 

* NASA TM X-53349 October 19, 1965 

AS-204 LAUNCH VEHICLE REFERENCE TRAJECTORY 

Robert M. Croft, Propulsion and Vehicle Engineering 

Laboratory. W. M. Gillis and T. W. Telfer, Aero-Astrodynamics 

Laboratory. 

NASA TM X-53319 August 16, 1965 

NASA TM X-53351 October 21, 1965 

CONIC SOLUTIONS TO THE INTERPLANETARY 

TRANSFER PROBLEM WITH CONSTANT OR 

MINIMUM INJECTION ENERGY 

AN ENVIRONMENTAL MODEL FOR VAN ALLEN 

BELT PROTONS 

Lamar E. Bullock, Aero-Astrodynamics Laboratory. William T. Roberts, Aero-Astrodynamics Laboratory. 

10 
SPACE SCIENCES (Coiitinued) 

NASA TM X-53354 November 1, 1965 NASA TM X-53406 March 8, 1966 

LAUNCH WINDOWS FOR TWO TYPES OF ORBITS 

SYNCHRONOUS WITH THE LUNAR PERIOD 

ORBITAL CALCULATIONS AND TRAPPED RADIATION 

MAPPING 

E. H. Bauer and L. D. Mullins, Aero-Astrodynamics 

Laboratory. Laboratory. 

M. 0. Burrell and J. J. Wright, Research Projects 

NASA TM X-53360 November 18, 1965 * NASA TM X-53408 March 9, 1966 

STATISTICAL ANALYSIS OF PHOTOGRAPHIC ME- AS-205 LAUNCH VEHICLE REFERENCE TRAJECTEOR DATA, PART II: VERNIANI'S LUMINOUS 

WEIGHTING 

Charles C. Dalton, Aero-Astrodynamics Laboratory. 

TORY 

J. W. Cremin, W. M. Gillis and T. W. Telfer, 

Aero-Astrodynamics Laboratory. 

EFFICIENCY AND SUPPLEMENTED WIIIrrLE 

NASA TM X-53375 December 29, 1965 NASA TM X-53417 March 24, 1966 

VELOCITY REQUIREMENTS FOR THE EARTH 

RETURN PHASE OF PLANETRAY MISSIONS 

Robert M. Jones and William T. Stephens, 

Propulsion and Vehicle Engineering Laboratory. 

SCIENTIFIC BASIS OF OBSERVATIONS FROM SPACE 

Dr. Alexander G. Smith, University of Florida, 

Research Projects Laboratory. 

NASA TM X-53434 April 12, 1966 

ANALYSIS OF AN INTERPLANETARY TRAJECTORY 

A 1975 VENUS FLYBY MISSION 

NASA TM X-53376 December 30, 1965 

SELF-SEALING SHIELDS FOR MICROMETEORITE TARGETING TECHNIQUE WITH APPLICATION TO 

PROTECTION 

Erwin D. Funk, Propulsion and Vehicle Engineering 

Laboratory. 

Bobby Ellison, Aero-Astrodynamics Laboratory. 

'k NASA TM X-53450 February 10, 1966 

SATURN I VEHICLE FLIGHT ANOMALY STUDY 

George Butler, Jr., Quality and Reliability Assurance 

Laboratory. 

NASA TM X-53385 February 1, 1966 

EARTH ORBITAL LIFETIME PREDICTION MODEL 

AND PROGRAM 

Ann R. McNair and Edward P. Boykin, Aero-Astrodynamics Laboratory. 

NASA TM X-53455 April 27, 1966 

NASA TM X-53399 

THE LUNAR ATMOSPHERE 

Wilmuth C. Lucas, Northrop Space Laboratories 

Otha H. Vaughan, Jr., Aero-Astrodynamics LaboraFebruary 23, 1966 CONTROL FACTORS FOR SATURN SA-203 

VEHICLE 

Billy W. Nunley , Aero-Astrodynamics Laboratory. 

tory. 
SPACE SCIENCES (Concluded) 

NASA TM X-53456 April 27, 1966 

AS-206A LAUNCH VEHICLE REFERENCE TRAJECTORY 

W. M. Gillis and T. W. Telfer, Aero-Astrodynamics 

Laboratory. 

NASA TM X-53470 June 3. 1966 

AS-202 LAUNCH VEHICLE OPERATIONAL FLIGHT 

TRAJECTORY 

NASA TN D-2944 November, 1965 

PHYSICS OF THE MOON - SELECTED TOPICS 

CONCERNING LUNAR EXPLORATION 

George C. Bucher and Henry E. Stern (Editors), 

Research Projects Laboratory. 

NASA TN D-2967 November, 1965 

APPLICATION OF AN ITERATIVE GUIDANCE MODE 

TO A LUNAR LANDING 

Pamelia B. Pack, Aero-Astrodynamics Laboratory. 

Helmut J. Horn, Aero-Astrodynamics Laboratory. 

NASA TM X-53472 June 6, 1966 

SATURN AS- 20 I/ APO L LO POST F LIGHT TRA JEC - 

TORY 

Jonathan B. Haussler and William G. Smith, AeroAstrodynamics Laboratory. 

NASA TN D-3244 February, 1966 

THEORETICAL RELATIONSHIPS FOR METEOROID 

PUNCTURE EXPERIMENTS 

Charles C. Dalton, Aero-Astrodynamics Laboratory. 

NASA TN D-3441 May, 1966 

APPLICATION OF UNITARY TRANSFORMATIONS 

TOFOURTHORDER PERTURBATIONTHEORY 

J. L. M. Cortez, Research Projects Laboratory, 

31 SPACE VEHICLES 

NASA TM X-53252 July 2, 1965 NASA TM X-53296 July 19, 1965 

MODIFIED LAUNCH VEHICLE (MLV) SATURN V 

IMPROVEMENT STUDY COMPOSITE SUMMARY VEHICLE 

RE PORT 

Compiled by Advanced Studies Office. 

CONTROL FACTORS FOR APOLM-SATURN 201 

Billy W. Nunley Aero-Astrodynamics Laboratory. 

NASA TM X-53298 July 21. 1965 

A PRACTICAL APPROACH TO THE OPTIMIZATION 

OF THE SATURN V SPACE VEHICLE CONTROL 

SYSTEM UNDER AERODYNAMIC LOADS 

Robert S. Ryan and Dieter Tcuber, Aero-Astrodynamics Laboratory. 

NASA TM X-53274 July 30, 1965 

TECIINIQUES OF IMPLEMENTING LAUNCH 

AUTOMATION I’ROGRAMS (SATURN IB SPACE 

VEIIICLE SYSTEM) 

William G. Bodic, Astrionics Laboratory. 
SPACE VEHICLES (Concluded) 

- NASA TM X-53300 

PEGASUS THERMAL DESIGN 

August 6. 1965 

Measuring and Evaluation Section. Propulsion and 

Vehicle Engineering Laboratory. 

NASA TM X-53374 1965 Tommy C. Bannister, Research Projects Laboratory. 

NASA TM X-53308 

RESEARCH ACHIEVEMENTS REVIEW SERIES NO. 6 

SA-8 FLIGHT TEST DATA REPORT 

"CONTROL SYSTEMS" 

August 2, 1965 

I 

NASA TM X-53338 September 30, 1965 

FINAL REPORT: DATA EVALUATION OF GROUND 

AND ENVIRONMENTAL MEASUREMENTS ON SA-8 

LAUNCH 

J. A. Lovingood and David N. Schultz, Aero-Astrodynamics Laboratory. 

H. J. Weichel, Aero-Astrodynamics Laboratory. 

NASA TM X-53311 September 14, 1965 NASA TM X-53380 January 21, 1966 

UTILIZATION OF AN ORBITAL LAUNCH FACILITY 

FOR PLANETARY MISSIONS 

Robert M. Croft, Propulsion and Vehicle Engineering 

AS-20 1 LAUNCH VEHICLE DYNAMICS ANALYSIS 

Elbert Sullivan, Dan McNiel, and Herschel Harmon, 

Aero-Astrodynarnics Laboratory. 

Laboratory. 

* NASA TM X-53381 January 25, 1966 

NASA TM X-53323 August 26, 1965 

SATURN IB IMPXOVEMENT STUDIES (PHASE I) 

EXECUTIVE SUMMARY REPORT 

C. R. ZimmermanandM. A. Page, Advanced Weiler, Aero-Astrodynamics Laboratory. 

Systems Office. 

AS-201 LAUNCH VEHICLE FLIGHT MECHANICAL 

SUMMARY 

0. M. Hardage, G. Wittenstein, P. Pack and J. 

NASA TM X-53405 March 8, 1966 

APOLLO EXTENSION SYSTEMS STUDIES REPORT 

NASA TM X-53326 September 3~ 1965 ON MFS/ LSSM JOINT USAGE STUDY 

N. R. Byrn, J. E. Ligocki, and J. T. Stanley, 

Northrop Space Laboratories. 

SUMMARY OF BASE THERMAL ENVIRONMENT 

MEASUREMENTS ON THE SATURN I BLOCK I 

FLIGHT VEHICLES 

March 24, 1966 Ira P. Jones, Jr., Aero-Astrodynamics Laboratory. NASA TM x-53418 

SPACE VEHICLE SA-8 TELEMETRY SYSTEM 

Telemetry Performance Evaluation Office, 

Astrionics Laboratory. 

Measuring and Evaluation Section, Propulsion and 

Vehicle Engineering Laboratory. 

NASA TM X-53345 October 7, 1965 

SA-10 FLIGHT TEST DATA REPORT 

Aero-Astrodynamics Laboratory. 

NASA TM X-53361 January 11, 1966 

FINAL REPORT: DATA EVALUATION OF GROUND 

u."-;y-c (continued) 

AND ENVIRONMENTAL MEASUREMENTS ON SA-10 

NASA TM X-53461 May 12, 1966 

PERCENTAGE LEVELS OF WIND SPEED DIFFERENCES COMPUTED BY USING RAWINSONDE WIND 

PROFILE DATA FROM CAPE KENNEDY, FLORIDA 

Dennis W. Camp and Michael Susko, Aero-Astrodynamics Laboratory. 

NASA TN D-3451 June, 1966 

PREDICTION OF PROPELLANT TANK PRESSURIZ AT ION REQUIREMENTS BY DIM E NSIONA L 

ANALYSIS 

13 
32 STRUCTURAL MECHANICS 

NASA TM X-53315 August 6, 1965 

COMPRESSION TESTS ON INTEGRALLY STIFFENED 

CYLINDERS 

Lester Katz, Propulsion and Vehicle Engineering 

Laboratory. 

NASA TM X-53355 November 1, 1965 

DISTRIBUTION OF FAILURE TIMES IN STRESS 

CORROSION TESTS 

J. B. Gayle, Propulsion and Vehicle Engineering 

Laboratory. 

NASA TM X-53359 November 17, 1965 

RANDOM VIBRATION ANALYSIS PROGRAM (RAVAN 

NASA TM X-53426 April 15, 1966 

EFFECT OF SOLAR-WIND BOMBARDMENT ON 

THERMAL CONTROL SURFACES 

Edgar R. Millcr, Research Projects Laboratory. 

NASA TM X-53440 April 20, 1966 

EXPLOSIVE CUTTING OF A MANHOLE IN SIMULATED SATURN V UPPER STAGE FUEL TANKS IN 

SPACE ENVIRONMENTS 

L. 0. Hamilton, Hayes International Corp., Manufacturing Engineering Laboratory. 

NASA TM X-53452 April 26, 1966 

PROBABILITIES OF ZERO WIND SHEAR PHENOMENA BASED ON RAWINSONDE DATA RECORDS 

Murl H. Newberry, Computation Laboratory. 

Lawrence E. Truppi, Aero-Astrodynamics Laboratory. 

ELASTIC STABILITY OF A SLENDER BAR WITH 

FREE-FREE ENDS UNDER DYNAMIC LOADS 

Frank C. Liu, Aero-Astrodynamics Laboratory. 

NASA TM X-53377 January 11, 1966 

, 

NASA TM X-53367 December 10, 1965 

NASA TM X-53457 May 2, 1966 

SATURN S-1-10 STATIC TEST VIBRATION *\ND 

ACOUSTIC DATA 

Measuring and Evaluation Section. Propulsion and 

Vehicle Engineering Laboratory 

NASA TM X-53382 January 27, 1966 

SATURN S-1-8 STATIC TEST VIBRATION AND 

ACOUSTIC DATA 

SATURN S-E3 STAGE VIBRATION AND ACOUSTIC 

ANALYSIS SA-25 STATIC TEST - SA-26 STATIC 

TEST 

Measuring and Evaluation Section, Propulsion and 

Vehicle Engineering Laboratory. 

NASA TN D-2941 August, 1065 

STRESS AND STRAIN DISTRIBUTIONS IN A THICICWALLED CYLINDER OF STRAIN-HARDENING 

MATERIAL, E LASTIC -PLASTIC A LLY STRAINED 

BY INTERNAL PRESSURE 

C. K. Liu, Professor of Mechanical Engineering, 

University of Alabama, University, Alabama, 

Structures Division. 

Measuring and Evaluation Section, Propulsion and 

Vehicle Engineering Laboratory. 

NASA TN D-2945 February, 1066 

NASA TM X-53387 February 2, 19G6 BLAST EFFECTS ON SPACE VElIICLE STRUCTURES 

THE EFFECT OF BENDING DYNAMICS AND CONTROL Reino Niemi and Richard Rnlwnau, Prcipulsion :mtl 

GAIN ON THE BENDING MOMENT Vehicle Engineering Lnl,uratory. 

Alberta C. King, Aero-Astrodynnmics Laboratory. 

14 
I' 

NASA TN D-3090 November, 1965 

VIBRATION ANALYSIS OF CLUSTERED LAUNCH 

VEHICLES 

Rudolf F. Glaser and Everette E. Beam, Propulsion 

and Vehicle Engineering Laboratory. 

NASA TN D-3387 April, 1966 

A GENERAL MATHEMATICAL MODEL FOR BEAM 

ANT) PTATE VIBRATION IN RENDING MODES USING 

LUMPED PARAMETERS 

I 3 STRUCTURAL MECHANICS (Concluded) 

33 THERMODYNAMICS AND COMBUSTION 

Irvin P. Vatz, Propulsion and Vehicle Engineering 

Laboratory. 

NASA TN D-3430 June, 1966 

TRANSIENT RESPONSE FROM THE LYAPUNOV 

STABILITY EQUATION 

William G. Vogt, Astrionics Laboratory. 

NASA TM X-53314 August 4, 1965 

SIZE AND DURATION OF FIREBALLS FROM PROPELLANT EXPLOSIONS 

J. B. Gayle and J. W. Bransford, Propulsion and 

Vehicle Engineering Laboratory. 

NASA TN D-3439 May, 1966 

EXPERIMENTAL MEASUREMENT OF OPTICAL 

ANGULAR DERIVATION CAUSED BY ATMOSPHERIC 

TURBULENCE AND REFRACTION. 

Robert L. Kurtz and James C. Hayes, Astrionics 

Laboratory. 

NASA TN D-3450 June, 1966 

A REVIEW OF SOME EXISTING LITERATURE 

CONCERNING DISCONTINUOUS STATE VARIABLES 

IN THE CALCULUS OF VARIATIONS. 

Rowland E. Burns, Aero-Astrodynamics Laboratory. 

Curtis R. Bailey, Propulsion and Vehicle Engineering 

Laboratory. 

NASA TN D-2750 July, 1965 

RADIATION GEOMETRY FACTOR BETWEEN THE 

EARTH AND A SATELLITE 

Tommy C. Bannister, Research Projects Laboratory. 

NASA TM X-53346 October 18, 1965 

A SET OF EXPERIMENTS IN THERMAL SIMILITUDE 

Billy P. Jones and James K. Harrison, Research 

Projects Laboratory. 

NASA TM X-53369 December 15, 1965 

A COMPILATION OF RADIANT AND CONVECTIVE 

HEATING TEST RESULTS 

F. Uptagrafft, L. A. Soileau, and T. Barkley, 

Propulsion and Vehicle Engineering Laboratory. 

NASA TM X-53371 December 20, 1965 

A PRELIMINARY INVESTIGATION OF OXIDIZER - RICH OXY GE N-HYDHUtiE N CGTviEX~~>? 

CHARACTERISTICS (continued) 

NASA TN D-2943 November, 1965 

A COLD GAS, SHORT DURATION TECHNIQUE FOR 

HIGH ALTITUDE, UNDEREXPANDED JET EXHAUST 

IMPINGEMENT STUDIES 

A. J. Gopin and E. L. Margolin, North American 

Aviation, Inc . , Aerodynamics Division, Aero-Astrodynamics Laboratory. 

NASA TN D-3153 December, 1965 

PERFORMANCE ANALYSIS OF CHEMICAL STAGES 

IN THE 300 TO 400 SECOND SPECIFIC IMPULSE 

RANGE FOR INTERPLANETARY MISSIONS 

Walter H. Stafford and Carmen R. Catalfamo, 

Propulsion and Vehicle Engineering Laboratory. 

15 
34 GENERAL 

NASA TM X-53282 October 20, 1965 

LAUNCH VEHICLE SAFETY ENGINEERING FOR 

STANDARD PAYLOAD MODULE 

Preston T. Farish, Industrial Operations 

NASA TM X-53373 1965 

RESEARCH ACHIEVEMENTS REVIEW SERIES NO. 

15 - 16 "ASTRODYNAMICS - GUIDANCE CONCEPTS" 

E. D. Geissler, Clyde Baker, C. C. Dearman, and 

Arthur Schwaniger, Aero-Astrodynamics Laboratory. 

NASA TM X-53299 July 22, 1965 

* NASA TM X-53392 December, 1965 

STANDARD PAYLOAD MODULE DEFINITION 

NETWORK FOR PHASES A, B, C, & D 

Preston T. Farish, Industrial Operations. 

SEMI-ANNUAL PROGRESS REPORT PART III - 

OSSA PROGRAM SUPPORTING RESEARCH 

PROJECTS 

Research Projects Iaboratory. 

NASA TM X-53305 July 26, 1965 

STANDARD PAYLOAD MODULE SYSTEM 

ANALYSIS PROCEDURES FOR SYSTEM DEFINITION 

Preston T. Farish, Industrial Operations. 

NASA TM X-53316 July 13, 1965 

* NASA TM X-53393 December, 1965 

SEMI-ANNUAL PROGRESS REPORT PART I - OART PROGRAM SUPPORTING RESEARCH 

PROJECTS 

Research Projects Laboratory. 

COST ESTIMATION FOR AEROSPACE PROJECTS * NASA TM X-53413 December, 1965 

Norman Levine, Aero-Astrodynamics Laboratory. 

NASA TM X-53357 November 4, 1965 

SIMULATION STUDY OF THE AMOUNT OF SENSITIVITY TEST DATA REQUIRED TO REJECT THE 

HYPOTHESIS OF NORMALITY WHEN THE SAMPLE 

POPULATION IS NONNORMAL 

J. B. Gayle and C. L. Hopkins, Propulsion and 

Vehicle Engineering Laboratory. 

SEMI-ANNUAL PROGRESS REPORT PART II - 

OMSF PROGRAM SUPPORTING RESEARCH 

PROJECTS 

Research Projects Laboratory. 
CONTRACTOR REPORTS 

CR - 350 November 3, 1965 

MINIMAX ATTITUDE CONTROL OF AEROBALLISTICS 

LAUNCH VEHICLES 

Hughes Aircraft Corporation, 

CR - 362 October 8, 1965 

A SUPERSONIC/HYPERSONIC AERODYNAMIC 

INVESTIGATION OF THE SATURN IB/APOLLO 

UPPERSTAGE 

David R. Carlson and William P. Walters, Northrop 

Space Iahoratories for Aero-Astrodymmics Lab. 

CR-6 1072 July 6, 1965 

A SUPERSONIC/ HYPERSONIC AERODYNAMIC 

INVESTIGATION OF THE SATURN IB/APOLLO 

UPPER STAGE 

David R. Carlson and William P. Walters, Northrop 

Space Labs, For Aero-Astraiynamics Lab., 

NAS 8-1111. 

CR - 61073 July 6, 1965 

A MATHEMATICAL MODEL FOR OPTIMIZING A 

MOLAB SURFACE MISSION 

J. M. Duffie, Jr., Brown Engineering Co., for 

Aero-Astrodynamics Lab. 

CR - 61074 Septemba: 7, 1965 

APOLLO EXTENSION SYSTEM STUDIES - TASK 

ORDER N-59 REPORT ON LEM APPLICATION TO 

LUNAR SHELTERS AND MOBILE VEHICLES 

Jerome E. Ligocki and Glenn J. Youngblood, 

Northrop Space Labs., for Propulsion and 

Vehicle Engineering Lab., NAS 8-11096. 

CR - 61075 July 6, 1965 

PARAMETRIC STUDY OF LUNAR LANDING 

TECHNIQUES USING A PREDETERMINED THRUST 

ORIENT AT ION 

Sam H. Harlin, Jr., Brown Engineering Co., for 

Propulsion and Vehicle Engineering Lab., 

NAS 8-20073. 

CR - 61077 July 13, 1965 

DESIGN STUDY OF SPECIAL PURPOSE SYSTEMS 

FOR THE LUNAR SURFACE 

P. J. Adinolfi and F, Z. Heinz, Jr., Hayes 

International corp., for Propulsion and Vehicle 

Engineering Lab., NAS 8-5307. 

CR - 61078 July 14, 1965 

VISUAL REQUIREMENTS BASED ON MINIMUM 

OBSTACLE AVOIDANCE DISTANCE 

R. T. IIeckman, Hayes Intcrnatianal Carp., for 

Propulsion and Vehicle Engineering Lab., NAS 8-5307. 

CR - 61079 July 29, 1965 

APOLLO EXTENSION SYSTEM PAYLOADS (MFS) 

KINESTHETIC EFFECTS 

D. W. Thomas, Northrop Space Labs., for AeroAstrodynamics Lab.. , NAS 8-20082. 

CR - 61080 August 9, 1965 

MESOSCALE STRUCTURE OF 11-20 KM WINDS 

A. T. Weinstein and E. R. Reiter, Meteorology 

Research, Inc., for Aerospace Environment Office 

Aero-Astrodynamics Lab. NAS 8-5294. 

CR - 61081 August 16, 1965 

RANDOM PROCESS THEORY AND PHYSICAL 

AQPLICAT IONS 

Georg' W. Bordner, et al., Cornel1 Aeronautical 

Laborah yy Inc. , NAS 8- 11346 for Computation Lab. 

CR - 61082 September 15, 1965 

METHODS OF FI'l "ING MULTIVARIANT FUNCTIONAL MODELS IN THL 4REA OF LARGE COMPUTER 

EXPLOITATION 

T. E. Perlin, et al., Georgia Institute of Technology 

NAS 8-5365 for Technology Utilization Office. 

17 
CONTRACTOR REPORTS (Continued) 

I' 

CR - 61083 September 23, 1965 

DATA COMPILATION AND EVALUATION OF SPACE 

SHIELDING PROBLEMS, VOLUME I: RANGE AND 

STOPPING POWER DATA 

C. W. Hill et at., Lockheed Nuclear Products, 

NAS 8-11164. 

CR - 61089 October 7, 1965 

ON THE NONLINEAR THEORY OF SANDWICH 

SHELLS 

Ibrahim K. Ebcioglu, University of Florida, 

NAS 8-5255. 

CR - 61090 September 24, 1965 

CR - 61084 September 23, 1965 

ADVANCED STUDIES OF STATIONARY PROCESSES: 

STATIONARITY, TESTING AND ASSOCIATED 

PROBLEMS 

Dr. M. X. Leadbetter et al., Research Triangle 

Institute, Durham, N. C., NAS 8-11316. 

A MONTE CARLO STUDY OF NEUTRON TRANSPORT 

THROUGH ALUMINUM, POLYETHYLENE AND 

CARBON SLABS 

M. 8. Wills, Radiation Research Associates, Inc., 

NAS 8-11047. 

CR - 61092 September 24, 1965 

CR - 61085 September 17, 1965 

FLUID AMPLIFIER DIGITAL INTEGRATOR 

A MONOGRAPH ON TORSIONAL VIBRATION MODES 

General Electric Co., NAS 8-5408. 

General Dynamics/Convair, NAS 8-114 - 86. 

CR - 61093 September 23, 1965 

CR - 61086 September 17, 1965 

PURE FLUID DEVICES 

SINGLE PARAMETER TESTING 

E. L. Berger and J. C. Jackson, G. E. Cdmpany - Daytona Beach, Florida, NAS 8-11715. 

D. W. Russel, Technical Director, Thrust Vector 

Control Study Group, Auburn University, NAS 8-2484. 

CR - 61094 September 24, 1965 

CR - 61087 September 24, 1965 

DESIGN OF AN OPTIMIZED VORTEX AMPLIFIER 

GUIDANCE SYSTEM ERROR STUDY 

Douglas Raney, et al, Northrop Space Labs., 

NAS 8-11431. 

Phillip E. Koerper, Case Institute of Technology, 

Cleveland, Ohio, NAS 8-11267. 

CR - 61095 October 1, 1965 

CR - 61088 September 23, 1965 

PRELIMINARY ERROR ANALYSIS OF A SPECTRUM 

MEASUREMENT SYSTEM 

David L. Finn, Georgia Institute of Technology, 

NAS 8-2473. 

INVESTIGATION OF ELECTROMC SWITCHES FOR 

ANALOG AND HYBRID COMPUTATION 

John W. Robertson, Georgia Institute of Technology, 

NAS 8-2473. 

CR - 61096 September 30, 1965 

DIRECT CURRENT BRUSHLESS TORQUER 

Dr. E. W. Martenfel, General Electric Co., 

NAS 8-11658. 

18 
I CONTRACTOR REPORTS (Continued) 

6 

CR - 61097 September 27, 1965 CR - 61103 October 18, 1965 

INVESTIGATION OF HIGH-ENERGY ELECTROMAGNETIC RADIATION EFFECTS ON SEMI-CONDUCTOR DEVICES A SURVEY OF SCIENTIFIC EXPERIMENTS AND 

INVESTIGATIONS FOR AES SHELTER-ROVING 

VEHICLE MISSIONS IN EXPLORATION OF THE 

MOON 

M. L. Anderson, Texas Instruments, Inc., 

NAS 5-5391. James T. Stanley and Wilmuth C. Lucas, Northrop 

Space Labs., NAS 8-11096. 

CR - 61098 September 27, 1965 

CR - 61105 November 9, 1965 

ON AXIOMS FOR HETEROGENEOUS CONTINUA 

ASPECTS OF STATISTICAL FILTER THEORY 

A. A. IIayday, University of Illinois (Project SQlJIl), 

Office of Naval Research - 1858(25) NR-098-038); 

work was completed by University of Alabama, 

Research Institute, NSG-381. 

Clemson University, S. C., NAS 8-11259. 

CR - 61106 November 17, 1965 

CR - 61099 September 23, 1965 LUNAR DUST/DEBRIS HAZARDS ASSOCIATED WlTH 

THE MANNED FLYING SYSTEM 

A THEORETICAL INVESTIGATION OF MU-CAPTURE 

RATES AND PROPERTIES OF COMPARABLE BETA 

TRANSlTIONS 

R. L. Stark, et al., Northrop Space Labs., 

NAS 8-20082. 

J. N. Huffaker, et ai., University of Alabama, 

NAS 8-11169. CR - 61107 November 17, 1965 

THE SCHEDULING OF MEASUREMENTS FOR ANALCR - 61100 September 27, 1965 YSIS OF AN ONBOARD NAVIGATION SYSTEM 

NONEQUILIBRIUM GASEOUS KINETICS (INTERIM 

RE PORT ) 

Paul J. Rohde, Philco Corporation, Palo Alto, 

Calif., NAS 8-11198. 

J. C. Pirkle, Jr., Georgia Institute of Technology, 

NAS 8-11242. CR - 61108 December 28, 1965 

ASTUDYOFFREE MOLECULARFLOWTHROUGH 

CR - 61101 September 30, 1965 VARIOUS LENGTH CYLINDRICAL NOZZLES 

MANNED FLYING SYSTEMS (MFS) CRYOGENIC 

ENGINES 

Walter J. Schaetzle, University of Alabama, 

NAS 8-5326. 

F. B. Tatom and L. M Bhalla, Northrop Space Labs., 

NAS 8-20082. CR - 61109 December 28, 1965 

CR - 61102 October 8, 1965 A STUDY OF FLUIDICS 

THE MOTION OF ASCENDING AND DESCENDING 

SPHERES 

Thrust Vector Control Study Group, Auburn University, 

NAS 8-20104. 

Paul B. MacCurdy, Jr. and Robbin E. Williamson, 

Meteorology Research, Inc., MRI 64 FR-210. 

19 
CONTR4CTOR REPORTS (Continued) 

CR - 61110 January 5, 1966 

A STUDY OF THE RELATIONSHIP OF CRYSTAL 

DEFECTS TO RELIABILITY OF EPITAXIAL 

SILICON PLANAR DEVICES 

H. J. John, et al., Westinghouse Electric Corp., 

Research Laboratories, NAS 8-11432. 

CR - 61111 January 11, 1966 

NEUTRON TRANSPORT DATA FOR SINGLE AND 

MULTILAYER SLABS OF ALUMINUM (POLYETHYTENE AND CARBON) 

M. B. Wells and J. M. Newell, Radiation Research 

Associates, Inc., NAS 8- 1 1047. 

CR - 61113 January 12, 1966 

COMPARISON OF SEVERAL ANALYTICAL SOLUTIONS 

TAL DATA 

TO THE SHEAR LAY PROBLEM WITH EXPERIMENDennis M. Rigsby, Bureau of Engineering Research, 

College of Engineering, University of Alabama, 

NAS 8-11155. 

CR - 61114 January 5, 1966 

THE X-TRANSFORM AND ITS USE IN SAMPLED 

DATA SYSTEMS ANALYSIS 

C . L. Phillips, Technical Director, Servomechanisms 

Laboratory, Auburn University. 

CR - 61115 January 11, 1966 

RESEARCH AND DEVELOPMENT IN THE FIELD 

OF PHYSICAL DETERMINATION OF MASS PROPERTIES 

Spaco, Inc., NAS 8-11314. 

CR - 61117 January 5, 1966 

INVESTIGATION TO DEFINE THE PROPAGATION 

CHARACTERISTICS OF A FINITE AMPLITUDE 

ACOUSTIC PRESSURE WAVE, PHASE I 

North American Aviation, Inc., Space & Information 

Systems Division, NAS 8-11441. 

CR - 61119 March 17, 1966 

IMPACT PRESSURE PROBE RESPONSE CHARACTERISTICS IN HIGH SPEED FLOWS, WITH TRANSITION KNUDSEN NUMBERS 

J. B. Wainright and K. W. Rogers, University of 

Southern California, Engineering Center, 

NAS 8-11046, 

CR - 61120 March 14, 1966 

SIP MATRIX INVERSION 

E. Y. Rodin, Wyle Laboratories - Research Staff , 

NAS 8-11217. 

CR - 61121 March 10, 1966 

THE VLASOV EQUATIONS 

Chih Kung Chov, Northrop Space Laboratories, 

NAS 8- 11440. 

CR - 61122 March 14, 1966 

MATHEMATICAL WIND PROFILES, PART IV 

Lockheed, NAS 8-5380. 

CR - 61123 March ii, 1966 

RESEARCH STUDIES OF RANDOM PROCESS THEORY 

AND PHYSICAL APPLICATIONS 

George W. Bordner, et al., Cornell Aeronautical 

Laboratory, NAS 8-11346. 

CR - 61124 March 14. 1966 

ANALYTICAL AND EXPERIMENTAL STUDIES OF 

RANDOM VIBRATION 

Paul Yu-fei Hu, California Institute of Technology, 

Dynamics, NAS 8-2451. 

20 
J 

CONTRACTOR REPORTS (Continued) 

r 

CR - 61125 March 11, 1966 CR - 61133 June 27, 1966 

JUNCTURE STRESS FIELDS IN MULTICELLULAR 

SHELL STRUCTURES, VOLUME III: STRESSES 

AND DEFORMATIONS OF FIXED-EDGE SEGMENTAL 

CONICAL SHELLS 

TRANSFER FUNCTION CURVE FIT STUDY - 7094 

COMPUTER PROGRAM NUMBER CQ 0005 

E. Correia, N. C. Adams, D. Hull, and F. M. Van 

Sickle, Space Division - Chrysler Corp. 

E. Y. W. Tsui, J. M. Massard, andP. Stern, TN-SE-65-45. 

Lockheed, NAS 8-11450. 

CR - 61134 June 28, 1966 

CR - 61126 March 14, 1966 

AZIMUTH AXIS OPTICAL ALIGNMENT SYSTEM 

FINA I, RE PORT 

- 

STUDY OF PTJRE FTJJID PHENOMENA, FINAL 

REPORT 

R. F. Brewster, G. C. Kuipers, W. W. Metheny, and 

J. N. Siebert, General Motors Corp. - Land Operations 

Dept., NAS 8-11649. 

Sperry Utah Company, Division of Sperry-Rand 

COT. , NAS 8-20102. 

CR - 61128 March 17, 1966 CR - 61135 June 24, 1966 

INCREMENTAL DIGITAL INTEGRATORS - FINAL 

REPORT 

AN INTRODUCTION TO ANALYTIC PLATFORMS 

FOR INERTIAL GUIDANCE 

Bunker - Ram0 Corp., Defense Systems Division, 

NAS 8-11608. 

Advanced Studies Group, Auburn University, 

NAS 8-20004. 

CR - 61129 April 12, 1966 CR - 61136 . June 28, 1966 

INTERPLANETARY NAVIGATION AND GUIDANCE 

STUDY, VOLUME 1: SUMMARY 

THE DETERMINATION OF ASYMPTOTIC AND 

PERIODIC BEHAVIOR OF DYNAMIC SYSTEMS 

ARISING IN CONTROL SYSTEM ANALYSIS - FINAL 

Philco Corporation, NAS 8- 11 198. REPORT 

E. Lefferts and E. Moshang, Martin Company, 

CR - 61130 April 11, 1966 NAS 8-20002. 

INTERPLANETARY NAVIGATION AND GUIDANCE 

STUDY, VOLUME II: TECHNICAL REPORT CR - 61137 June 28, 1966 

Philco Corporation , NAS 8-11198. PARAMETER OPTIMIZATION - INTERIM REPORT 

George D. Cole, University of Alabama, NAS 8-5411. 

CR - 61131 April 11, 1966 

INTERPLANETARY NAVIGATION AND GUIDANCE 

STUDY, VOLUME III: ILLUSTRATIONS AND TABLES 

CR - 61139 June 28, 1966 

STUDY OF THE METHODS FOR THE NUMERICAL 

SOLUTION OF ORDINARY DIFFERENTIAL EQUATIONS 

- FINAL REPORT 

Philco Corporation, NAS 8- 11198. 

CR - 61132 June 27, 1966 0. B. Francis, Jr., L. J. Gallaher, J. M. Gwynn,, Jr., 

H. G. Hale, .Jr., T. E. Perlin, and W. T. Wall - Engineering Esperiment Station - Georgia Tech, 

NAS 8-20014. 

ROCKETDYNE CROSS - SPECTRAL ANALYSIS 

COMPUTER PROGRAM 

hl. R. .Dubman and B. J. Byars, Rocketdyne Corp., 

Study Authorization No. GO51 - 0081. 

21 
CR - 61140 

* , CONTRACTOR REPORTS (Concluded) 

June 28, 1966 CR - 61142 4 

June 28, 1966 

A STUDY OF ERROR APPROXIMATION FOR 

HYBRID COMPUTERS 

AN ANALYTICAL STUDY OF SEPARATED FLOW 

ABOUT A CIRCULAR CYLINDER 

Joseph L. Hammond, Jr., School of Electrical 

Engineering - Georgia Tech, NAS 8-2473. 

R. H. Vjihara, R. F. Stevenson, and F. C. Hung 

North American Aviation, Inc., NAS 8-20140. 

CR - 61141 June 28, 1966 

THE GENERATION OF A GAUSSIAN RANDOM 

PROCESS IN A POSITION PARAMETER 

David L. Finn and W. A. Yates, School of Electrical 

Engineering, Georgia Tech, NAS 8-2473. 

22 
*- 

ARTICLES, PAPERS ,AND PRESENTATIONS 

By George C. Marshall Space Flight Center Personnel 

Aberg, John W. R-P& VE-VA 

SYSTEMS ENGINEERING AND RELATED ASPECTS 

IN PROPULSION AND VEHICLE ENGINEERING 

Oral Presentation to the Swedish Interplanetary 

Society at Stockho:m, Sweden, September, 1965. 

Aberg, JohnW R-P& VE-VA 

SA'1'UKN/APO LLO PROJECT 

Oral presentation to the Swedish Interplanetary 

Society at Stockholm, Sweden, August 31, 1965. 

Bartee, Ed R-AS 

A METHOD FOR SELECTING AND ORDERING 

LUNAR EXPERIMENTS ACCORDING TO SCIENTIFIC 

MERIT 

Paper presented to the 29th Annual Meeting of the 

Operations Research Society of America, at Santa 

Monica, California, May 18-20, 1966. 

Baughcr, Charlos R. R-RP-F 

THE FARADAY ROTATION AND DISPERSIVE 

DOPPLER EFFECTS IN THE IONOSPHERE AT 

OBLIQUE INCIDENCE 

Master Thesis for the University of Missouri. 

Bannister, T. C. R-RP-T 

RESEARCH AND DEVELOPMENT STUDY ON SPACE 

THERMAL CONTROL BY USE OF FUSIBLE 

MATERIALS 

Papers presented to the 1966 Institute of Environmental Sciences at San Diego, California, April 

13-15, 1966. 

Baugher, Charles R. R-RP-F 

MEASUREMENTS OF THE IONOSPHERIC ELECTRON 

CONTENT BY MEANS OF THE IONOSPHERE BEACON 

SATELLJTES 

Oral presentation to the Rocket City Astronomical 

Association, Huntsville, Alabama, July 29, 1965. 

Bannister, T. C. R-RP-T 

PEGASUS THERMAL CONTROL COATINGS EXPERIMENT 

Paper presented to the 4th Aerospace Sciences Conference of AIAA at Los Angeles, California, June 

27-29, 1966. 

Beal, James B. R-QUAL-.4MR 

NONDESTRUCTIVE TESTING APPLIED TO ADHESIVE BONDED STRUCTURES 

Oral presentation,to the SAMPE Meeting at Huntsville, 

Alabama, April 4, 1966. 

Barnett, Donald 0. P& VE-PTP 

Beal, James B. R-QUAL-AMR 

THERMAL STRATIFICATION OF A CRYOGENIC 

FLUID IN A PARTIALLY FILLED SPHERICAL 

CONTAINER 

Master Thesis for the University of Alabama. 

INCREASING RELIABILITY OF BONDED STRUCTURES 

BY USE OF N. D. T. 

Oral presentation to the IEEE Reliability Group 

Meeting at Huntsville, Alabama, May 26, 1966. 

23 
c 

ARTICLES, PAPERS, AND PRESENTATIONS (Continued) I 

Beyerle, F. R-ME-MMC Broussard, P. H. 

4 R-ASTR-GCB I 

MANUFACTURING AND HANDLING PROCEDURES 

FOR PLANETARY SPACECRAFT TO BE STERILIZED 

BY HEATING BEARING 

Paper presented to CAL-TECH, Pasadena, California, 

March, 1966. at San Francisco, California, October 18-20, 1965. 

THEORY AND EXPERIMENTS OF SQUEEZE-FILM 

GAS BEARING - PART I: 

I ,CYLINDRICAL JOURNAL 

I 

Paper presented to the ASME-ASLE Joint Conference 

Blumrich, J. F. R-P& VE-SA Brown, E. R-ME-M 

STUDIES IN ADVANCED SPACE VEHICLE 

CONTAINERS 

Paper presented to the SAE Conference at Huntsville, 

Alabama, June 14-16, 1966. 

ONE SIDE BONDED COMMON BULKHEAD 

Paper presented to the Adhesive Conference at 

Huntsville, Alabama, March 19, 1966. 

Burns, R. E. R-AERO-GO 

AN ANALYTICAL REDUCTION OF THE OPTIMAL 

TRAJECTORY PROBLEM 

Master Thesis for University of Alabama. 

Bombara, E. L. I-E-Q 

DECISION PROCEDURE FOR MINIMIZING COSTS 

OF CALIBRATION LIQUID ROCKET ENGINES 

Paper presented to the 11th Conference on the 

Design of Experiments in Army Research, Development and Testing, at Hoboken, New Jersey, October 

21. 1965. Cataldo, C. E. R-P& VE-MM 

MATERIALS IN SPACE EXPLORATION 

Bradford, Lynn R-AS-P Oral presentation to the National Association of 

MOBILITY AIDS FOR LUNAR SURFACE EXTRA- October 21, 1965. 

VEHICULAR ACTIVITY 

Corrosion Engineers at New Orleans, Louisiana, 

Oral presentation to the National Conference on 

Space Maintenance and Extra-vehicular Activity, Cataldo, C. E 

at Orlando, Florida, March 1-3, 1966. 

METALS RESEARCH 

R-P& VE-MM 

Oral presentation to the U.S. Navy Reserve Officers 

Brenneckc, Margaret, W. R-ME-M Seminar at Huntsville, Alabama, May 15, 1966. 

ALUMINUM WELDING METALLURGY AS RELATED 

TO OUR USE IN MANUFACTURING 

Paper prcscnted to the Symposium of American 

Welding Research Council, at Birmingham, Alabama, 

Octolwr 6, lN5. OF LARGE SPACE STRUCTURES EMPLOYING 

Crawford, Ron R-AS-V 

STRUCTURAL WEIGHT AND COST COMPARISON 

BERY LLIUM-ALUMINUM ALLOYS 

Paper presented to the AIAA Conference at Orlando, 

Florida, April 18-20, 1966. 
n ARTICLES, PAPERS, AND PRESENTATIONS (Continued) 

Crawford, Ron R-AS-V 

DESIGN CRITERIA FOR TYPICAL PLANETARY 

SPACECRAFT TO BE STERILIZED BY HEATING 

Oral presentation to the National Conference on 

Spacecraft Sterilization Technology at Pasadena, 

California, November 16-18, 1965. 

Crawford, Ron R-AS-V 

DESIGN REQITTREMENTS FOR STERILIZATION 

CONTAINEKS OF SANITARY LANDERS 

Oral presentation to the Second Annual Meeting and 

Technical Demonstration, AIAA, at San Francisco, 

California, July 26-29, 1965. 

Dalton, Charles C. R-AERO-Y 

VELOCITY DEPENDENCE OF METEOR LUMINOUS 

EFFICIENCY AND CONSEQUENT STATISTICAL 

RESULTS 

Paper presented to the AIAA Conference at Los 

Angeles, California, June 27-29, 1966. 

Dearman, Jr., C. C. R-AERO-G 

FIRST ORDER SECULAR PERTURBATIONS OF AN 

AliTIFICIAL EARTH SATELLITE DUE TO TIIE SUN 

AND MOON 

Oral presentation to the 3rd Southeastern Conference 

on Theoretical and Applied Mechanics at Columbia, 

South Carolina, March 31-April 1, 1966. 

Dalins, Dr. I. R-RP-N 

Demorest, Keith, E. R-P& VE-MEE 

SMALL GLASS SYSTEMS - A COMPARISON WITH 

METAL SYSTEMS 

Oral presentation to the NASA High Vacuum Technology 

Testing, and Measurement Meeting at Lewis Research 

Center, Cleveland, Ohio, June 8-9, 1965. 

THE EFFECT OF VARIOUS LUBRICANTS AND BASE 

MATERIALS ON FRICTION AT ULTRA HIGH MADS 

Oral presentation to the Joint ASLE-ASME Conference 

at San Francisco, California, October 18-20, 1965. 

Dalins, Dr. I. R-RP-N Dendy, W. F. R-QUA L-OT 

SOME SPECIAL DESIGNS FOR UHV APPLICATIONS QUALITY ASSURANCE TRAINING PROGRAM 

Paper presented to the NASA High Vacuum Technology, 

Testing, and Measurement Meeting at Lewis Research 

Center, Cleveland, Ohio, June 8-9, 1965. 1966. 

Oral presentation to the Research Seminar for Naval 

Reserve Officers at Huntsville, Alabama, May 13- 15, 

Dalton, Charles, C. R-AERO-Y Drummond, Floyd, M. I-E-J 

INFERENCES FROM PHOTOGRAPHIC METEORS LAUNCH VEHICLE ENGINE DEVELOPMENT 

Oral Presentation to the Symposium on Meteor Orbits 

and Dust at Cambridge, Massachusetts, August 9-13, 

1965. 1966. 

Oral presentation to the Student Space Symposium, 

University of Missouri at Rolla, Montana, March 25, 

25 
ARTICLES, PAPERS,AND PRESENTATIONS (Conti1,Led) 

Dyer, M. K. R-QUA L-Q Farmer,Dr. Richard C. R-AERO-AT 

PRODUCT "TRACEABILITY" FOR NASA SPACE 

SYSTEMS 

Oral presentation to the 20th Annual Technical 

Conference and Exhibit ASWC at New York City, 

June 1, 1966. Springs, Colorado, June 13-17, 1966. 

THE VERIFICATION OF A MATHEMATICAL MODEL 

WHICH REPRESENTS LARGE, LIQUID ROCKETENGINE EXHAUST PLUMES 

Oral presentation to the AIAA Conference at Colorado 

Felker, K. J. R-AERO-YS 

Edmondson, N. R-RP-N 

ASPECTS OF MATHEMATICS AS APPLIED TO 

PHYSICS 

Oral presentation at LeMoyne College, Memphis, 

Tennessee, December 23, 1965. 

DECREASE IN ELECTRON DENSITY IN THE 

IONOSPHERE FOLLOWING THE PASSAGE OF 

SATURN I 

Paper presented to the AIAA Conference at Miami 

Beach, Florida, January 24-26, 1966. 

Fields, Stanley R-RP-T 

Ely, 0. P. R-ASTR-IRD 

RADIO PROPAGATION EFFECTS OF ROCKET 

EXHAUST PLASMAS 

Paper presented to the International Space Electronic 

Symposium at Miami Beach, Florida, November 2-4, 

1965. 1966. 

THE BEHAVIOR OF SIMULATED LUNAR MATERIALS 

IN AN ULTRAHIGH VACUUM ENVIRONMENT 

Paper presented to the 43rd Annual Meeting of the 

Alabama Academy of Sciences at Birmingham 

Southern College, Birmingham, Alabama, April 1-2, 

Evans, Herbert R -T E ST -T 

GAS TURBINE POWERED TOWBOAT (CLERMONT 

DESIGN. DEVELOPMENT AND EARLY OPERATING 

EXPERIENCE) 

Oral presentation to the Society of Naval Architects 

and Marine Engineers at Houston, Texas, February 

11, 1966. 

Farish, Dr. Preston T. I-RM-F 

THE SYSTEM SAFETY OBJECTIVES AS RELATED 

TO MANAGEMENT BASELINES 

Paper presented to the Configuration Management 

Symposium sponsored by the American Society for 

Quality Control, Philadelphia, Pennsylvania, November 19, 1965. 

Fnrish, Dr. Preston T. I- ItM - F 

THE INSPECTOR IN TliE MANNED FLIGHT AWARENESS PROGRAM 

Fisher, Dr. Carl D. R-P& VE-VAH 

IN FLIGHT STERILIZATION OF MASS PROBES 

Paper presented to the AIAA Conference at Baltimore, 

Maryland, March 29, 1966. 

Fountain, J. A. R-RP-T 

THE IMPROVED GUARDED COLD PLATE THERMAL 

CONDUCTIVITY APPARATUS 

Paper presented to the 5th Conference on Thermal 

Conductivity at Denver, Colorado, October 22, 1965. 

Fritz, C. G. R-P&VE-PEC 

BUBBLE COALESCENCE IN A LONGITUDINALLY 

VIBRATED LIQUID COLUMN 

Paper presented to the ASME Conference at Chicago, 

Illinois, November 7, 1965. 

Oral presentation to American Society for Quality 

Control Annual Meeting at New York, New York, 

June 3, 1966. 

26 
r 

n ARTICLES, PAPERS, AND PRESENTATIONS (Continued) 

Hamiter, L. C. R-QUA L-RP 

Fritz, C. G. R-P&VE-PEC 

DYNAMICS AND MOTION OF BUBBLES IN A LIQUID 

Oral presentation to the graduate Seminar,Purdue 

University, Lafayette, Indiana, February 16, 1966. 

Goldston, R. L. I-RM-M 

DATA MANAGEMENT AT MARSHALL SPACE 

FLIGHT CENTER 

Oral presentation to the 8th Annual Meeting of AOA 

at Daytona Beach, Florida, April 28, 1966. 

Goldston, R. L. I-RM-M 

APOLLO DATA MANAGEMENT 

Oral presentation to Data Management Executives, 

Daytona Beach, Florida, April 28, 1966. 

Graham, John MS-T 

COMMERCIAL UTILIZATION OF SPACE AGE 

DE VE LOPMENTS 

Oral presentation to the Textile Data Processing 

Association at Jekyll Island, Georgia, May 1-3, 1966. 

Grubbs, H. Y. R-P& VE-VA 

NASA LUNAR SURFACE VEHICLE SIMULATOR -- 18 DAY SIMULATED MANNED LUNAR SCIENTIFIC 

MISSION 

Oral presentation to the AIAA Meeting at Bedford, 

Massachusetts, May 17, 1966. 

Grubbs, H. Y. R-P& VE-VA 

MANNED LUNAR SURFACE VEHICLE DESIGN 

CRITERIA 

Oral presentation to the 7th Annual Symposium on 

Human Factors and Electronics, Minneapolis, 

Minnesota, May 5, 1966. 

THE FAST SCANNING INFRARED MICROSCOPE, 

A NEW DIMENSION IN INFRARED NONDESTRUCTIVE 

TESTING 

Oral presentation to the 25th National Convention of 

the Society for Nondestructive Testing at Detroit, 

Michigan, October 18-22, 1965. 

Hamiter, L. C. R-QUAL-RP 

FAST SCANNING INFRARED MICROSCOPE FOR 

SEMI-CONDUCTOR EVALUATION 

Paper presented to the IEEE Conference at New York, 

New York, March 23, 1966. 

Harris, Ronald J. R-AS-VP 

A MODULAR NUCLEAR VEHICLE SYSTEM WITH 

MULTI-MISSION CAPABILITY FOR MARS STOPOVER MISSIONS 

Paper presented to the AIAA Meeting at Colorado 

Springs, Colorado, June 13-15, 1966. 

Hill, Kelly R-AERO-YE 

ANALYSIS OF DETAILED WIND PROFILES FOR 

THE LAUNCH OF SATURN AS-201 ON FEBRUARY 

26, 1966 

Paper presented to the AIAA/AMS Joint Conference 

at Los Angeles, California, March 28-April 1, 1966. 

Hooper, J. W. R-COMP-S 

TIMING CONSIDERATIONS B 5500 ALGOL 

Oral presentation to the Spring Meeting of Cooperating 

Users of Burrough's Equipment (CUBE) at Atlanta, 

Georgia, April, 1966. 

27 
ARTICLES, PAPERS, AND PRESENTATIONS (Continued) 

Hopson, G. D. R-P& VE-PTD 

ROCKET ENGINE CLUSTERING AND VEHICLE 

INTEGRATION AS INFLUENCED BY BASE THERMAL 

ENVIRONMENTS 

Oral presentation to the 2nd Propulsion Specialist 

Conference, AIAA, Colorado Springs, Colorado, 

June 13, 1966. 

Horn, H. J. R-AERO-D 

THE ITERATIVE GUIDANCE LAW FOR SATURN 

Oral presentation to the AIAA Meeting at Baltimore, 

Maryland, October 27-29, 1965. 

Horton, J. C. P& VE-MEV 

WEAR AND NOISE CHARACTERISTICS OF BRUSHCOMMUTATOR CONTACTS IN HIGH VACUUM 

Oral presentation to the 3rd International Research 

Symposium on Electrical Contact Phenomena at the 

University of Maine, Orono, Maine, June 6-10, 1966. 

Huffaker, R. M. R-AERO-ATP 

INHOMOGENEOUS RADIANT HEAT TRANSFER FROM 

H-i, F-1, 5-2 ROCKET EXHAUST PLUMES 

Oral presentation to the 2nd Propulsion Specialist 

Conference, AM, Colorado Springs, Colorado, 

June 13, 1966. 

Huffaker, R. M. R-AERO-ATP 

CURRENT RESEARCH ON INFRARED RADIATION 

FROM ROCKET EXHAUST 

Hunt, Robert M. R-P& VE-S 

SATURN V GROUND WINDS PROGRAM 

Paper presented to the Meeting on Ground Wind 

Problems in Relation to Launch Vehicles at 

Langley Research Center, Hampton, Virginia, June 

6, 1966. 

Hurst, C. W. R-AERO-GG 

EARTH TO MOON TRAJECTORY FOR MAXIMUM 

TERMINAL MASS 

Master Thesis for the Auburn University, Auburn, 

Alabama. 

Jones, Billy P. R-RP-T 

THEORY OF THERMAL SIMILITUDE WITH APPLICATIONS TO SPACECRAFT 

Article published in Astronautica Acta, Summer, 1966. 

Jones, Ira P. R-AERO-AT 

SUMMARY OF SATURN I BASE THERMAL ENVIRONMENT 

Article published in the Journal of Spacecraft and 

Rockets, April, 1966. 

Jones, R. P. R-AERO-AM 

A MONTE CARLO APPROACH TO TRANSITION AND 

FREE MOLECULAR FLOW PROBLEMS 

Paper presented to the 5th InterMtiOMl Symposium 

on Rarefied Gas Dynamics at Oxford, England, 

June, 1966. 

Oral presentation to the Symposium on Interdisciplinary Aspects of Radiative Energy Transfer at 

Philadelphia, Pennsylvania, February 24-26, 1966. 

28 
c ARTICLES, PAPERS ,AND PRESENTATIONS (Continued) 

.' 

King, J. (Co-Author) R-RP 

STUDY OF NERVA ELECTRIC MANNED MARS 

VEHICLE 

Paper presented to the Radio-Isotope Application in 

Aerospace Symposium at Dayton, Ohio, February 

14-16, 1966. 

Kingsbury, James E. R-P& VE-M 

MATERIALS AND TOOLS FOR SPACE RESEARCH 

Oral prtscntntinn to the Annual Tndiistrial Arts 

Conference at Lakeland, Florida, November 7, 1965. 

Krause, Dr. F. R. A-AERO-AM 

Krause, Dr. F. R. A-AERO-AM 

CONVECTIVE HEAT TRANSFER IN TURBULENT 

SUPERSONIC BASE FLOW 

Paper presented to the AIAA Specialist Conference 

on the Aero-Therm0 Chemistry of Turbulent Flows 

at San Diego, California, December 13-15, 1965. 

Kuers, Dr. W. R. R-ME-DIR 

MANAGEMENT OF SATURN/APOLLO MANUFACTURING EFFORTS 

Oral presentation to the Society of Automotive 

Engineers at Los Angeles, California, October 

4-8, 1965. 

THE CROSSED-BEAM CORRELATION TECHNIQUES 

Lindberg, J. P. R-AERO-F 

Paper presented to the AIAA Specialist Conference 

on the Aero-Therm0 Chemistry of Turbulent Flows 

at San Diego, California, December 13-15, 1965. 

SATURN I FLIGHT TEST EVALUATION 

Paper presented to the Joint AIAA/ASME Meeting 

at the University of Tennessee, Knoxville, Tennessee, 

April 27, 1966. 

Krause, Dr. F. R. A-AERO-AM 

REMOTE SENSING WITH OPTICAL CROSS CORRELATION METHODS 

Oral presentation to the AAP Symposium at Huntsville, 

Alabama, January 12, 1966. 

Krause, Dr. F. R. R-AERO-AM 

OPTICAL INTEGRATION OVER CORRELATION 

AREAS IN TURBULENT FLOWS 

Paper presented to the 5th International Congress on 

Acoustics at Liege, Belgium, September 7-14, 1965. 

Krause, Dr. F. R. R-AERO-AM 

A TECHNIQUE FOR THE MEASUREMENT OF LOCAL 

TURBULENT PROPERTIES IN SUPERSONIC SHEAR 

LAYERS 

Lovingood, J. A. R-AERO-G 

CONTROL SYSTEMS FOR THE SATURN LAUNCH 

VEHICLES 

Article published in Aeronautics/Astronautics, May, 

1966. 

Lowe, E. G. R-ASTR-G 

SLIP RING CAPSULE ASSEMBLY DEVELOPMENT 

AND RELIABILITY FOR SATURN GUIDANCE 

PLAT FORMS 

Paper presented to the Symposium on Precision, 

Sliding Contact Devices at Roanoke, Virginia, 

November 3, 1965. 

Papers presented to the 5th International Congress on 

Acoustics at Liege, Belgium, September 7-14, 1965. 

29 
ARTICLES, PAPERS,AND PRESENTATIONS (Continued) . 

Lucas, Dr. W. R. R-P& VE-DIR 

COMPOSITE MATERIALS FOR LAUNCH SHELL 

STRUCTURES 

Paper presented to AIAA Conference at San Francisco, 

California, July 26, 1965. 

Marsalis, W. E. R-TEST-B 

TEST LABORATORY'S CRYOGENIC STORAGE AND 

TRANSFER FACILITIES 

Oral presentation to the Tennessee Valley Chapter of 

the Cryogenic Society of America, Huntsville, 

Alabama, June 30, 1966. 

Lucas, Dr. W. R. R-P& VE-DIR 

Mathur, Dr. S. C. R-P& VE-MEV 

DEVELOPMENT OF NONDESTRUCTIVE TESTING 

TECHNIQUES FOR SATURN HONEYCOMB HEAT 

SHIELDS 

Paper presented to the Metals/Materials Congress 

at Detroit, Michigan, October 18-22, 1965. 

Lucas, Dr. W. R. R-P& VE-DIR 

THE PAST, PRESENT, AND FUTURE OF METALS 

FOR LIQUID ROCKETS 

Paper presented to the Metals/Materials Congress 

at Detroit, Michigan, October 18-22, 1965. 

Lucas. Dr. W. R. R-P& VE-DIR 

METAL-METAL COMPOSITE - A NEW STRUCTURAL 

MATERIAL 

Paper presented to the 7th AIAA/ASME Joint 

Conference on Structures and Materials at Cocoa 

Beach, Florida, April 18-20, 1966. 

SIMPLE LCAO-MO CALCULATIONS FOR HYDROGEN PHTKLOCYANE 

Article published in Journal of Chemical Physics, 

June, 1966. 

Mathur, Dr. S. C. R-P& VE-MEV 

MAGNETIC BEHAVIOR OF NI' ION IN THE CRYSTAL 

OF NICKEL ACETATE TERA-HYDRATE 

Article published in Vol. 31 of Physica. 

McCampbell, W. R-ME-ME 

THE DEVELOPMENT OF A WELD INTELLIGENCE 

SYSTEM 

Paper presented to the American Welding Society 

Conference at Birmingham, Alabama, October 4-7, 

1965. 

McDonough, Dr. G. F. R-AERO-D 

Lucas. Dr. W. R. R-P& VE-DIR 

DEVELOPMENT OF FOAMED CERAMIC-METAL 

HONEYCOMB COMPOSITES FOR RADIANT HEATING AND VIBRATIONAL ENVIRONMENTS 

Paper presented to the AIAA Conference at 

Washington, D. C., May 7-12, 1966. 

3 0 

NON-LINEAR DYNAMICS OF AN ARTIFICIAL 

GRAVITY ORBITING SYSTEM 

Oral presentation to the 5th U.S. National Congress 

of Applied Mechanics at the University of Minnesota, 

Minneapolis, Minnesota, June 14-15, 1966. 
ARTICLES, PAPEFC3,AND PRESENTATIONS (Continued) 

Mrazek, Dr. W. A. I- DIR Parks, Gordon P. R-ME-MW 

MANNED SPACE AND LUNAR EXPLORATION OUT-OF-VACUUM ELECTRON BEAM WELDING 

Oral presentation to the Saturn Manufacturing Review 

Meeting at The Boeing Company, Michoud, Lousiana, 

May 23, 1966. 

Paul, David R-AS-VL 

Oral presentation to the Aerospace Workshop of the 

University of Hawaii at Honolulu, Hawaii, June 17, 

1966. 

THECHALLENGEOFALTERNATEAPPROACHES 

TO THE ACHIEVEMENT OF LUNAR EXPLORATION 

AND EXPLOITATION 

Naumann, Dr. Robert J. R-RP-P 

RECENT NASA METEOROID PENETRATION RESULTS 

FROM SATELLITES Paper presented to the National Aeronautic and 

Space Engineering and Manufacturing Meeting at 

Los Angeles, California, October 4-8, 1965. Paper presented to the International Symposium on 

Meteor Orbits and Dust at Cambridge, Massachusetts, 

August 9-13, 1965. 

OIConnor, Edmund, F. I-DIR 

Perry, Davis R-ASTR-NFS 

THE SATURN LAUNCH VEHICLES 

ACTUATOR PRATICIPATION IN A BENDING MODE 

Oral presentation to the AIAA Conference at San IDENTIFICATION SYSTEM 

rrarlciacv, ciilZ~y;i=, Jn'y ?G, 196.5. 

O'Connor, Edmund, F. I-DIR Paper presented to the SAE Meeting at New Orleans, 

Louisiana, January 19-21, 1966. 

SATURN VEHICLES FOR THE APOLLO PROGRAM 

Oral presentation to the AIAA Regional Meeting at 

St. Louis, Missouri, October 11, 1965. Peskar, R. E. R-P& VE-SVR 

UTILIZATION OF THE SATURN S-IC BOOSTER AS 

AN ACOUSTIC SOURCE 

O'Connor, Edmund, F. I- DIR Paper presented to the Acoustics Society of America 

Symposium at St. Louis, Missouri, October, 1965. THREE STEPS TO SPACE 

Oral presentation to the Society of Professional 

Engineers at Huntsville, Alabama, May 13, 1966. 

Orillion, A. G. R-P& VE-AV 

Platt, G. K. R-P& VE-PTF 

SPACE VHEICLE LOW GRAVITY FLUID MECHANICS 

PROBLEMS AND THE FEASIBILITY OF THEIR 

EXPERIMENTAL INVESTIGATION 

SELECTED METHODS FOR UPRATING SATURN 

VEHICLES 

Oral presentation to the Advanced Launch Vehicle 

and Propulsion Systems Conference at Huntsville, 

Alabama, June 14-16, 1966. 

Master Thesis for the University of Alabama. 

Rees, Eberhard, F. DEP-T 

MSFC APPROACH IN ACHIEVING HIGH RELIABILITY 

OF SATURN CLASS VEHICLES 

Paludan, C. T. R-ASTR-IM 

Paper presented to 4th Annual Reliability and 

Maintainability Conference at Los Angeles, California, I 

July 28-30, 1965. 

LEAK RATE INSTRUMENTATION FOR SATURN 

SYSTEMS 

Paper presented to the Aerospace Systems Conference 

at Seattle, Washington, June il-14, 1966. 

32 
ARTICLES, PAPERS, AND PRESENTATIONS (Continued) 

McDonough, Dr. G. F. R- AE RO - D Middleton, R. L. R-P& VE-PT 

STABILITY PROBLEMS IN THE CONTROL OF 

SATURN LAUNCH VEHICLES MSFC 

CRYOGENIC INSULATION DEVELOPMENT AT 

Paper presented to the International Conference on 

Dynamic Stability of Structures at the Northwestern 

University, Evanston, Illinois, October, 1965. 1966. 

Oral presentation to the Huntsville Chapter of the 

Cryogenic Society at Huntsville, Alabama, January, 

McDonough, Dr. G. F. R-AERO-D Miller, J. L. R-ASTR-EAP 

LIQUID FREE SURFACE INSTABILITY IN VERTICAL 

RANDOM EXCITATION SPACE APPLICATION 

THE CAPILLARY MATRIX FUEL CELL FOR AEROPaper presented to the 6th International Symposium 

on Space Technology and Science at Tokyo, Japan, New Orleans, Louisiana, June 11-15, 1966. 

November 29-December 4, 1965. 

Paper presented to the IEEE Power Confercncc at 

Mrazek, Dr. W. A. I-DIR 

LAUNCH VEHICLE SYSTEM ENGINEERING AND 

TECHNOLOGICAL PROBLEMS 

McDonough, Dr. G. F. R-AERO-D 

DYNAMIC TESTING OF SATURN LAUNCH VEHICLES 

Paper presented to the 6th International Symposium on 

Space Technology and Science at Tokyo, Japan, 

November 29-December 4, 1965. 

Oral presentation to the German Society for Rockctry 

and Spaceflight at Munich, Germany, July 19-22, 1965. 

Mrazek, Dr. W. A. I-DIR 

SATURN/APOLLO PROGRAM 

McKannan, E. C. R-P& VE-MEE 

DIELECTRICS IN SPACE APPLICATIONS 

Oral presentation to the Society of Aerospace 

Oral presentation to the Working Group on Extraterrestrial Resources at Colorado Springs, Colorado, 

Materials and Aerospace Engineers at Huntsville, November 30, 1965. 

Alabama, February 14, 1966. 

Mrazek, Dr. W. A. I-DIR 

OUR FUTURE IN SPACE -- THE SATURN FAMILY 

McKay, Jr., G. H. R-P& VE-PPE 

PROBLEMS ARISING FROM CURRENT TRENDS IN 

PROPULSION SYSTEM DESIGN AND GUIDANCE 

SCHEMES at Deer Park, New York, January 12, 1966. 

Oral presentation to the Long Island Section of AIAA 

Paper presented to the AIAA Propulsion Specialists 

Conference at Colorado Springs, Colorado, June, Mrazek, Dr. W. A. I-DIR 

1966. 

SATURN CLASS VEHICLES 

Oral presentation to the Palm Bcach Section of AIAA 

at Palm Beach, Florida, March 9, 1966. 

31 
ARTICLES, PAPERS, AND PRESENTATIONS (Continued) 

Reinfelds, Juris R-RP 

APPLICATION OF AN APPROXIMATE SOLUTION 

OF PARTIAL WAVE DISPERSION RELATIONS TO 

YAKAWA POTENTIAL SCATTERLNG 

Article published inThe Physical Review, June, 1966. 

Rheinfurth, M. H. R-AERO-DC 

A NEW APPROACH TO THE EXPLANATION OF 

FLUTTER MECHANISM 

Paper presented to the AIAA Symposium on Structural 

Dynamics and Aero Elasticity at Boston, Massachusetts, 

August 30-September 1, 1965. 

Ritter, Glen R-ASTR-FA 

STATUS OF PILOTED GUIDANCE AND CONTROL 

STUDIES FOR THE SATURN V LAUNCH VEHICLES 

Paper presented to the SAE Conference at New 

Orleans, Louisiana, January 19-21, 1966. 

Roberts, W. T. R-AERO-YS 

CHEMILUMINESCENT MEASUREMENTS OF UPPER 

ATMOSPHERIC WINDS 

Paper presented to the AIAA Meeting at San Francisco, 

California, July 26-29, 1965. 

Roberts, W. T. R-AERO-YS 

Ruppe, Harry R-AS 

THE EXPLORATION OF MARS AND VENUS 

Paper presented to the National Meeting of the 

American Astronomical Society at Blackburg, 

Virginia, August 23-27, 1965. 

Rushing, H. W. R-QUA L-PI 

INSTRUMENTATION SYSTEM SIGNAL CONDITIONER 

GAIN CHANGE, OFFSET, AND DRIFT CUMPENSATION BY COMPUTER 

Paper presented to the Southeastern Conference of 

the EA, Augusta, Georgia, April 20, 1966. 

Ryan, R. S. R-AERO-DD 

A TECHNIQUE FOR ANALYZING CONTROL GAINS 

USING FREQUENC;Y Kr;SPuiGE iviEYXGZ2 

Oral presentation to the AIAA Meeting at Los Angeles, 

California, June 27-29, 1966. 

Saunders, Grady R-ASTR-I 

THE AROD SYSTEM 

Paper presented to the 10th Symposium on Space and 

Ballistic Missile Technology at San Diego, California, 

August 4-6, 1965. 

DECREASE IN ELECTRON DENSITY IN THE 

IONOSPHERE FOLLOWING THE PASSAGE OF 

SATURN I 

Schaefer, Herbert R-AS-P 

Paper presented to the ALL4 Conference at Miami 

Beach, Florida, January 24-26, 1966. 

Rochelle, W. c. R-AERO-ATB 

THEORETICAL AND EXPERIMENTAL INVESTIGATION OF HEATING FROM SATURN SOLID PROPELLANT ROCKET EXHAUST 

Paper presented to the AIAA Meeting at Colorado 

Springs, Colorado, June 13-17, 1966. 

TESTING OF LUNAR SURlACE VEHICLES UNDER 

SIMULATED LUNAR GRAVITY CONDITIONS 

Paper presented to the SAE Conference at Detroit, 

Michigan, January 10-14, 1966. 

Schmidt, D. M. R-QUAL-PC 

AUTOMATIC CHECKOUT SYSTEMS FOR STAGES 

OF THE SATURN V MANNED SPACE VEHICLE 

Oral presentation to the IEEE International Convention at New York City, New York, March 21, 1965. 
ARTICLES, PAPERS ,AND PRESENTATIONS (Continued) 

Schock, Richard W. R-P& VE-SVE 

A SURVEY OF SHOCK AND VIBRATION ENVIRONMENTS IN THE FOUR MAJOR MODES OF TRANSPORTATION 

Paper presented to the 35th Symposium of Shock, 

Vibration and Associated Environments at New 

Orleans, Louisiana, October 27-29, 1965. 

Schwinghamer, R. J. R-ME-M 

NEW DEVELOPMENTS IN MAGNETOMOTIVE 

FORMING, AND A NEW CONCEPT - MAGNETO - HYDRAULIC FORMING 

Paper presented to the ASME Design Engineering 

Conference at Chicago, Illinois, May 9-12, 1966. 

Seitz, R. N. R-COMP-DIR 

Schock, Richard W. P-P& VE-SVE 

A SURVEY OF SHOCK AND VIBRATION ENVIRONMENTS 

Paper presented to the 35th Shock and Vibration 

Symposium, New Orleans, Louisiana, October 26, 

1965. 

Schuerer, P. H. R-ME-MMP 

AEROSPACE APPLICATION OF FUSED SILICA 

CERAMIC TOOLING 

Oral presentation to the Southeastern Section of the 

American Ceramic Society's Quarterly Meeting at 

Gatlingburg, Tennessee, July 8-10, 1965. 

Schuerer, P. H. R-ME-MMP 

EXPLOSIVE FORMING 

Paper presented to the Engineering Institute at the 

University of Wisconsin, Madison, Wisconsin, 

March 10-11, 1966. 

Schuler, A. E. R-TEST-ID 

THE ROLE OF WEIGHING IN THE DEVELOPMENT 

AND FIRING OF MISSILES AND SPACE SHIPS 

Paper presented to the National Scale Men's Association Conference at Atlanta, Georgia, April 25-28, 

1966. 

Schwinghamer, R. J. R-ME-M 

TOOL EXPERIMENTS FOR ASSEMBLY, MAINTENANCE AND REPAIR IN SPACE 

Oral presentation to the National Conference on 

Space Maintenance and Extra-Vehicular Activity at 

Orlando, Florida, March 2, 1966. 

AMTRAN, A REMOTE - TERMINAL, CONVERSATIONAL-MODE COMPUTER SYSTEM 

Oral presentation to the Mid-Southeastern Chapter 

ACM Meeting at Huntsville, Alabama, February 11, 

1966. 

Shame, Mitchell R. I-DRR 

MANNED FLIGHT AWARENESS--ZERO DEFECTS 

FOR MAN-RATED SPACE VEHICLES 

Article published in Industrial Quality Control, No. 6, 

June, 1966. 

Shelton, Dr. R. D. (Co-author) R-RP-N 

STUDY OF NERVA ELECTRIC MANNED MARS 

VEHICLE 

Paper presented to the Radio-Isotope Application in 

Aerospace Symposium at Dayton, Ohio, February 

14-16, 1966. 

Shelton, Dr. R. D. R-RP-N 

CRITICAL STORMER CONDITIONS IN QUADRUPLE 

AND DOUBLE RING CURRENT FIELDS 

Article published in the Journal of Mathematical 

Physics, Vol VI, No. 12, December, 1965. 

Smith, 0. E. R-AERO- Y-'E 

PROGRESS IN CIRCUMVENTING LIMlTATIONS OF 

UPPER WIND RECORDS 

Article published in the Journal for Applied Meteorology, Vol V, No. 3, June, 1966. 

34 
ARTICLES, PAPERS,AND PRESENTATIONS (Continued) 

Smith, 0. E. R-AERO-Y-T 

AN ACOUSTIC WIND MEASUREMENT TECHNIQUE 

Paper presented to the AIAA Conference at Los 

Angeles, California, June 27, 1966. 

Teuber, D. L . R-AERO-RM 

METHODS FOR MEASURING THE SENSITIVITY OF 

A LAUNCH VEHICLE CONTROL SYSTEM ON THE 

ANALOG COMPUTER 

Oral presentation to the Inter-Center Workshop on 

Analog-Hybrid Computation at Langley Research 

Center, September, 1965. 

Smith, 0. E. R-AERO-Y-T 

MISSILE RANGE REFERENCE ATMOSPHERES-- 

THEIR ORIGIN AND USE 

Paper presented to the 6th National Conference of 

Applied Meteorology at Los Angeles, California, 

March 28-31, 1966. 

Thompson, Zack R-ASTR-NFS 

ACTUATOR PARTICIPATION IN A BENDING MODE 

IDENTIFICATION SYSTEM 

Paper presented to the SAE Meeting at New Orleans, 

Louisiana, January 19-21, 1966. 

Snoddy, W. C. R-RP-T 

Turner, R. E. R-AERO-Y 

IRADIATION ABOVE THE ATMOSPHERE DUE TO 

RAYLEIGH SCATTERING AND DIFFUSED TERRES- 

'I MnL KfiI! hfib L LVI. - ---- 

Paper presented to the AIAA Thermo-Physics 

Specialists Conference at Monterey, California, 

September 13-15, 1965. 

Snoddy, W. C. R-RP-T 

PROBLEMS IN THE THERMAL DESIGN OF 

SPACECRAFT 

Oral presentation to the AIAA Thermo-Physics 

Snecialists Conference at Monterey, California, 

September 13-15, 1965. 

LIGHTWEIGHT TRANSPONDESONDE 

Article published in the American Meteoroiogicai 

Society's Bulletin, June, 1966. 

Turner, Robert E. R-AERO-Y 

MSFC ATMOSPHERIC MEASURING STATIONS 

Article published in the American Meteorological 

Society's Bulletin, February, 1966. 

Vaughn, 0. H. R-AERO 

ENGINEERING SURFACE MODELS FOR LUNAR 

MOBILmY DESIGN CRITERIA 

Steinberg, A. I-E-Q 

RELIABILITY AND QUALITY MANAGEMENT 

Paper presented to the International Lunar Geological 

Conference at Bend, Oregon, August 22-29, 1965. 

Oral presentation to the Virginia Polytechnical 

Institute at Blacksburg, Virginia, January 11, 1966. 

Vaughn, 0. H. R-AERO 

Stuhlinger, Dr. Ernst (Co-author) R-RP-DIR 

STUDY OF A NERVA ELECTRIC MANNED MARS 

VEHICLE 

Paper presented to the Radio-Isotope Application in 

Aerospace Symposium at Dayton, Ohio, February 14- 

16, 1966. 

TEMPORAL COLOR ENHANCEMENTS ON THE 

MOON 

Paper presented to the Southeastern Section of the 

American Physical Society at Charlottesville, Virginia, 

November, 1965. 
ARTICLES, PAPERS. AND PRESENTATIONS (Continued) 

von Braun, Wernher DIR 

THE APOLLO MANNED SPACE FLIGHT PROGRAM 

Oral presentation to the XVI International Astronautical 

Congress at Athens, Greece, September 12-18, 1965. 

von Braun, Wernher DIR 

MANNED LUNAR LANDING PROGRAM - PROJECT 

APOLLO 

Oral presentation to the 11th Annual Seminar of the 

American Society for Industrial Security at Atlanta, 

Georgia, October 12-14, 1965. 

von Braun,, Wernher DIR 

PROSPERITY THROUGH SPACE COMPETENCE 

Oral presentation to Students and Faculty of the 

University of Miami at Coral Gables, Florida, 

November 3, 1965. 

von Braun . Wernher DIR 

LAUNCH VEHICLES 

Panel discussion member, 1965 International Space 

Electronics Symposium at Miami Beach, Florida, 

November 2-4, 1965. 

von B,raun, Wernher DIR 

THE NEXT 20 YEARS OF INTERPLANETARY 

EXPLORATION 

Article published in Aeronautics and Astronautics, 

November, 1965. 

von Braun, Wernher DIR 

THE TIME FOR SPACE EXPLORATION 

Article published in IEEE Spectrum, December, 1965. 

Walker, R. D. I-PL-PC 

SATURN VEHICLE CRYOGENIC PROGRAMS 

Paper presented to the 1965 Cryogenic Engineering 

Conference at Houston, Texas, August 23-25, 1965. 

Wells, Ernest B. R-RPJ 

SCIENCE AND RELIGION 

Oral presentation to the Professional Men Section of 

the Methodist Church, Huntsville, Alabama. 

Wheeler, John T. R-AERO-X 

APPLICATION OF HIGHER-ORDER RUNGE-KUTTA 

INTEGRATION TECHNIQUE DEVELOPED BY DR. 

ERWIN FEHLBERG TO LOW-THRUST TRAJECTORIES 

Master Thesis for the University of Alabama. 

Wilson, H. B. R-AERO-AT 

A SHORT-DURATION TECHNIQUE FOR SIMULATED 

ROCKET EXHAUST AND WIND TUNNEL FLOW AND 

lTS APPLICATION 

Paper presented to the Heat Transfer and Fluid 

Mechanics Institute at the University of Santa Clara, 

Santa Clara, California, June 22-24, 1966. 

Winstead, T. W. R-P& VE-PTP 

THERMAL CONTROL OF LIQUID H2/02 ROCKET 

ENGINES AND VEHICLE IMPACT 

Paper presented to the AIAA Conference at Colorado 

Springs, Colorado, June 13- 17, 1966. 

Woodcock, G. R. (Co-Author) R-AS-VL 

STUDY OF NERVA ELECTRIC MANNED MARS 

VEHICLE 

Paper presented to the Radio-Isotope Application in 

Aerospace Symposium at Dayton, Ohio, February 

14-16, 1966. 

Woodcock, G. R. R-AS-VL 

CAPABILITY OF SATURN V TO SUPPORT MARS 

EXPLORATION 

Paper presented to the New York Academy of Sciences 

Conference at New York City, Nevi York, November 

3-4, 1965. 

36 
ARTICLES, PAPERS, AND PRESENTATIONS (Concluded) 

Worlund, A. L. R-P&VE-PTF Wyatt, G. L. MS-F 

THEREDUCTIONOFPOGOEFFECTSBYGAS 

INJECTION SAFETY PROBLEMS 

SPACE VEHICLE DEVELOPMENT - ASSOCIATED 

Paper presented to the AIAA Conference at Colorado 

Springs, Colorado, June 13-17, 1966. Aerospace Section, at Chattanooga, Tennessee, 

Paper presented to the Southern Safety Conference, 

March 6-8, 1966. 

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