”? b 

-6. . + 

NASA Technical Memorandum 86998 

A Bibliography of Electrothermal 

Thruster Technology, 1984 

James S. Sovey and Terry L. Hardy 

Lewis Researcb Center 

Cleveland, Ohio 

Matthew Englehart 

Paper Basics 

Brookpark, Obi0 

NASA 

National Aeronautics 

and Space Administration 

Scientific and Technical 

Information Branch 

1986 
CONTENTS 

Page 

SUMMARY ........................ 1 

INTRODUCTION ...................... 1 

DESCRIPTION OF THE BIBLIOGRAPHY ............ 2 

CONCLUDING REMARKS ................... 2 

BIBLIOGRAPHY 

Category 1 . Resistojets ............... 4 

Category 2 . Arcjets ................. 16 

Category 3 . Related Toplcs ............. 23 

Category 4 . Propellent Management .......... 33 

Category 5 . Power and Control ............ 34 

Category 6 . Pulsed Electrothermal Engines ...... 36 

Category 7 . RF and Microwave Devices ........ 37 

Category 8 . Solar Thermal Thrusters ......... 38 

Category 9 . Laser Thermal Propulsion ........ 39 

AUTHOR INDEX ...................... 41 
A BIBLIOGRAPHY OF ELECTROTHERMAL THRUSTER TECHNOLOGY, 1984 

James S. Sovey and Terry L. Hardy 

National Aeronautics and Space Administration 

Lewis Research Center 

Cleveland, Ohio 44135 

and 

Matthew Englehart 

Paper Basics 

Brookpark, Ohio 

SUMMARY 

Electrothermal propulsion concepts are briefly discussed as an introduction to a bibliography and author index for resistojets, thermal arcjets, 

pulsed electrothermal t h r u s t e r s , m i c r o w a v e heated devices, solar thermal 

thrusters, and laser thermal thrusters. 

INTRODUCTION 

Electrothermal propulsion systems have characteristics that are attractive for geosynchronous satellite stationkeeping, altitude maintenance for low 

Earth orbiting spacecraft, maneuvering, and orbit raising. Electrothermal 

thrusters comprise resistojets, thermal arcjets, pulsed electrothermal thrusters, microwave heated devices, solar thermal thrusters, and laser thermal 

thrusters (figs. 1 to 6). 

Resistojets (fig. 1) use resistive elements to heat the propellant and, 

thus, increase exhaust velocity. Potential propellants for resistojets 

include nitrogen, ammonia, hydrogen, carbon dioxide, steam, and mixtures of 

carbon dioxide or methane and hydrazine. Resistojet propulsion is the most 

mature technology of those discussed herein. 

ments and operational propulsion systems using resistojets were developed from 

1965 to 1984. In 1984, 40 hydrazine resistojets are performing north/south 

stationkeeping on 8 Intelsat V and 3 RCA spacecraft (refs. 01:225:1981 and 

01:234:1983). NASA is now pursuing the development of a permanent facility in 

low Earth orbit. This facility will comprise a manned space station core, 

co-orbiting platforms, and free-flying spacecraft which require propulsion 

systems for orbit maintenance, maneuvering, and possibly attitude control. 

The resistojet system is a candidate to satisfy these auxiliary propulsion 

requirements, which are more demanding and variable than those of present 

space systems. 

Approximately 26 flight experiThe thermal arcjet (fig. 2) converts electrical energy to thermal energy 

by using an arc discharge. The thermal energy is further changed to directed 

kinetic energy by expanding the propellant through a nozzle. Thermal arcjets 

for space propulsion were the object of significant technology efforts from 

about 1959 to 1965. Today, a renewed interest in the arcjet rests on its 

potential for high-performance stationkeeping systems, for satellite propulsion, and for high-power orbit raising applications. 
Exploratory stud 

pulsed electrothermal 

thermal (ref. 08:003: 

Technology work deals 

potential. 

es and some experimental evaluations have been made for 

(ref. 06:003:1984), microwave (ref. 07:012:1984), solar 

983), and laser thermal (ref. 09:019:1982) devices. 

primarily with concept feasibility and performance 

This report is a bibliography of the work related to the six types of 

electrothermal thrusters as well as to power processing and propellent management. An author index of all citations is also included. 

DESCRIPTION OF THE BIBLIOGRAPHY 

This bibliography is designed to give the technologist and systems engineer an extensive list of reports relating primarily to resistojet and thermal 

arcjet technology. A significant number of citations deal with propellent 

management, power systems, and other electrothermal propulsion concepts. 

There are nine separate categories under which the reports are listed: 

resistojets, thermal arcjets, related topics, propellent management, power and 

control, pulsed electrothermal thrusters, RF and microwave devices, solar 

thermal thrusters, and laser thermal thrusters. The entries are listed in an 

order such that the chronological order of the year of publication supersedes 

the alphabetical order of the author's last name. Each entry has a threenumber code. The first number of the code is the category number. For example, resistojets are category one, and laser thermal thrusters are category 

nine. The category number is followed by the number of that particular entry 

within the category. The third number of the code is the year in which the 

report was published. This code permits easy location of each author's publication through the author index found at the end of the bibliography. 

CONCLUDING REMARKS 

The bibliography contains nearly 700 citations relating primarily to 

low-thrust (4 N), electrothermal propulsion system technology. Included in 

the bibliography are three survey papers on electric propulsion (01:230:1982), 

01:235:1983, 01:239:1984), three survey papers relating primarily to resistojets and arcjets (02:106:1965, 01 :181:1973, 01 :231:1982), and one survey paper 

on laser research and applications (09:022:1983). Other papers summarize the 

performance, design criteria, and technology status for electrothermal thrusters, power processors, and propellent system components. Many papers deal 

with mission analysis, system studies, propulsion system design, thruster 

materials, propellent properties, diagnostic methods, flow field effects, and 

nozzle performance. The bibliography has been designed to facilitate updating. 

2 
r Cathode 

Prop9llant 

1.. 

Figlire 1. - Resistojet. I 

,r Containment tube 

,-Cathole ,' 1z0 Yozzle 7 

I ; ,-Consumable liner / 

/ 

I' 

\ '\ Polyethylene 

\ liner 

Hnoae 

Figure 3. - Pulsed electrothermal thruster. 

Heat exchanger 

cavity (absorber) 

Heat exchanger cavity 

(windowless) 

Figure 5. - Solar thermal thruster. 

I 

r Anod? 

iUozzle 

Constrictor \ 

Propellent 

injector 

Figlire 2. -Thermal arcjet. 

Power 

Microwave 

gsnerator 

Dissociation -., 

'4 

'\ - 

Expansion - 

Laser 

bean 

I) 

Figgre 4. - Microwave heated device. 

[TKz509sec 

I 

/ 

/ 

/ I 

Focusing Hydrogon 

lens plasma 

Figure 6. - Laser thermal thruster. 

b 

3 
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01:OlO: 1963 

01 : 01 1 : 1964 

BIBLIOGRAPHY 

Category 1 - Resistojets 

Theoretical Performance of Propellants 

Suitable for Electrothermal Jet Engines. 

Jack, J.R. 

NASA TN D-682, 1961. 

Regenerative and Radiation Cooling of 

Electrothermal Thrust Generators. 

Jack, J.R. 

Preprint 61-97-1791, hrican Rocket Society, 

June 1961. 

Investigation of Electric Resi stance-tleated 

Rocket for Feasibility in Space Propulsion 

&pl i cations. 

Howard, J.H. 

ASD-TR-62-487, June 1972. 

The Resistojet. 

Howard, J.H. 

ARS J., 1962, pp. 961-962. 

Elect-Thermal Rocket. 

Jack, J.R.; beckel, W.E. 

Patent No. APPL-SN-58147, United States, 1962. 

Electrothermal Propulsion Prospects. 

Page, R.J. 

ARS Paper 264942, American Rocket Society, 

Nov. 1962. 

Survey of the Status of Electrothermal Propulsion fmn Engine Development Viewpoint 

and Discussion of Arc Jet and Resistojet 

Engi nes . Page, R.J. 

ARS Paper 62-2649, American Rocket Society, 

Nov. 1962. 

Electrothermal Engine Research and 

Development. 

Avco Corp. NASA CR-101661, 1963. 

Research on Electrothermal Thrustor for 

Attitude Control Systems. 

Braberg, H.L.; Jeffries, N.P.; Cunbers, L. 

General Electric. Co. ASD-TDR-63-816, 

Aug. 1963. 

NASA Research on Resistance Heated Hydrogen 

Jets. 

Jack, J.; Spisz. E. 

AIAA Paper 63-023, Mar. 1963. 

Electrothermal Engine Research and 

Development, Phase I. 

RAD-TR-64-32, Avco Corp. NASA CR-54104, 1964. 

01:012:1964 

01:013:1964 

01:014:1964 

01:015:1964 

01:016:1964 

01:017:1964 

01:018:1964 

01:019:1964 

01:020:1964 

01:021:1965 

01:022:1965 

4 

Development of a Milowatt Resistojet. 

Bennett, 5.; Clark, K.E.; Connors, J.F. 

AIAA Paper 64-672, Sept. 1964. 

Resistojet Research and Development - Phase 11. 

Bennett, 5.; John, R.R. 

Avco Corp. NASA CR-54155, 1964. 

Resistance Heated Thrustor Research. 

Ducati, A.C.; Huehlberger, E.; Todd, J.P. 

AFAPL-TR-65-71, Giannini Scientific Corp., 

July 1965. 

Electrothermal Propulsion Testing Techniques. 

Ducati, A.; Huehlberger, E.; Todd, J.P. 

AIAA CP-11, 1964. 

Research on Resistanceaated Thrustors. 

Jack, J.R.; Spisz, E.W. 

NASA TN D-2281, 1981. 

Analytical Methods for Resistance Jet Design. 

Jeffries, N.P. 

General Electric Co. NASA CR-67322, 1964. 

Analytical Evaluation of Possible 

Noncryogenic Propellants for Electrothermal 

Thrusters. 

Schaefer, J.W.; Ferrante, J. 

NASA TN 0-2253, 1964. 

Resistance Heated Thrustor Research. 

Todd, J.P. 

APL-TDR-64-45, Giannini Scientific Corp., 

Jan. 1964. 

Analytical Methods for Resistance Jet Design. 

Viventi, R. 

General Electric Co. NASA CR-84823, 1964. 

Experimental Propulsion Performance of a Low 

Power Pulsed Resistojet. 

Bennett, 5.; Huss, W.; John, R.R.; Tuchman, A. 

AIAA Paper 65-97, Jan. 1967. 

Recent Advances in Electrothermal and Hybrid 

Electrothermal-Electromagnetic Propulsion. 

Bennett, 5.; John, R.R. 

Symposium on Advanced Propulsion Concepts, 

4th, Palo Alto, CA, Apr. 26-28, 1965, USAF 

Office of Scientific Research, Apr. 1965. 
01 :023: 1965 

01 :024: 1965 

01:025:1965 

01:026: 1965 

01:027: 1965 

01:028:1965 

01:029:1965 

01 :030: 1965 

01:031:1965 

01:032:1966 

01:033: 1966 

01:034: 1966 

Electrothermal Rockets Having Uproved Heat 

Exchangers. 

Brinich, P.F.; Jack, J.R. 

Patent No. APPL-SN-313132, United States, 1965. 

Resistance Heated Thruster Research. 

Ducati, A.C.; fluehlberger, E.; Todd, J.P. 

Gianinni Scientific Corp. AFAPL-TR-65-71, 

July 1965. 

Resistojet Research and Developnent - Phase 11. 

John, R.R.; Morgan, D. 

RAD-SR-65-44, Avco Corp . NASA CR-54333, 

Jan. 1965. 

Resistojet Research and Developnent - 

Phase 11. 

John, R.R. 

RAD-TR-65-13, Avco Corp. NASA CR-54330, 1965. 

Resistojet Research and Development. 

Phase I1 

John, R.R. 

Avco Corp. NASA CR-101656, 1965. 

The Design and Performance of a 3-kU 

Concentric Tube Resistojet. 

Page, R.J.; Short, R.A. 

1X-25168, Marquardt Corp. NASA CR-54410, 

1965. 

Thrust Coefficients of Low-Thrust Nozzles. 

Spisz, E.W.; Brinich, P.F.; Jack, J.R. 

NASA TN 03056, 1965. 

The Developnent of Resistance Jet Thruster 

Viventi, R. 

General Electric Co. NASA CR-67550, 1965. 

Systems. 

Research and Investigation of a Resistance 

Jet Attitude Control System. 

Wells, R.C.; Viventi, R.E. 

General Electric. AFFDL-TR-65-140, Nov. 1965. 

Design, Development, Fabrication, Test and 

Delivery of Electrothermal Engine Systems. 

Avco Corp. NASA CR-103470, 1966. 

Design, Developnent, Fabrication, Test and 

Delivery of Electrothermal Engine Systems. 

Avco Corp. NASA CR-78103, 1966. 

Resistojet Propulsion System for Spacecraft 

Control. 

Avco Corp. NASA CR-83264, 1966. 

01:035: 1966 

01:036: 1966 

01:037:1%6 

01:036:1966 

01 :039: 1966 

01:040: 1966 

01:041:1966 

01 :042: 1966 

01:043: 1966 

01:044:1966 

Recent Advances in Electrothermal and Hybrid 

Electrothermal-Electramgnetic Propulsion. 

Bennett, S.; John, R.R. 

United Aircraft Corp. Advanced Propulsion 

Concepts, 1966, pp. 125-154. 

Experimental and Analytical Evaluation of 

Electrotheml and Electromagnetic Space 

Propulsion Engines. 

Bennett, S.; John, R.R. 

Proc. 17th Int. Astronautical Congress, 

International Astronautical Federation, 

Oct. 1966. 

Progress and Prospects of Electrical 

Propul si on. 

Ernstene, fl.P. 

AIM Paper 66-830, Nov. 1966. 

The Potentialities of Electric Propulsion in 

the Near Future. 

Fabri, J.; Le Grives, E.; Surugue, J. 

ONERA-TP-394, Office National d'Etudes et de 

Recherches Aerospat iales, 1966. 

Advanced Low-Thrust Propulsion Systems for 

Station Keeping and Stability Control of the 

NASA Manned Orbital Research Laboratory 

(HORL) Resistojets and Radioisotope 

Thrusters. 

Gooctnan, H. 

AIM Paper 66-226, Mar. 1966. 

3 kU Concentric Tubular Resistojet 

Performance Canpared with Theory. 

Halbach, C.R.; Page, R.J.; Short, R.A. 

AIM Paper 66-224, Har. 1966. 

An Operational Electrothermal Propulsion 

System for Spacecraft Reaction Control. 

Jackson, F.A.; et al. 

AIM Paper 66-213, Har. 1966 

Resistojet Research and Development. 

Phase I1 - Supplement No. 1. 

John, R.R. 

Avco Corp. NASA CR-72123, 1966. 

Design, Development, Fabrication, Test and 

Delivery of Electrothermal Engine Systems. 

John, R.R. 

AVSSD-0362-66-CRI Avco Corp. 

1966. 

NASA CR-72 104, 

Resistojet Research and Development. 

Phase I1 - Design, Developnent and 

Fabrication of an Amnonia-Fueled Resistojet 

Thrustor System. 

John, R.R. 

AVSSO-0356-66-CR, Avco . Corp . NASA CR-54688, 

1966. 

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01:051:1967 

01:052:1967 

01:053:1967 

01:054:1967 

01:055:1967 

A Resistojet System for Attitude Control Of 

Umnned Earth Satel 1 i tes. 

Kosson, R.L.; Tobias, 1.1. 

AIAA Paper 66-225, Mar. 1966. 

Lou Thrust Nozzle Performance. 

Murch, C.K.; Silver, A.H.; Marcisz, T.J. 

AIM Paper 68-91, Jan. 1966. 

3 kW Concentric Tubular Resistojet 

Performance. 

Page, R.J.; Halbach, C.R.; Short, R.A. 

J. Spacecr. Rockets, vol. 3, no. 11, Nov. 

1966, pp. 1669-1674. 

Report on the Development of the Manned 

Orbiting Research Laboratory (FURL) System 

Improvement Study. 

Pisciotta, A. 

SH-488196, Douglas Aircraft Co., Jan. 1966. 

Integration and Launch Support and Part 

Flight Analysis of the Resistojet Thrustor 

System on ATS-8. 

Avco Corp. NASA CR-89503, 1967. 

On the Application of Electric Propulsion to 

Satel 1 i te Orbit Adjustment and Station 

Keeping . Barrett, C.C. 

NASA TH X-55880, 1967. 

Design and Performance of a Thermal Storage 

Resi stojet . Cygnarowicz, T.A.; Gibson, R.N., Jr. 

NASA TM X-55884, 1967. 

Design and Performance of a Thermal Storage 

Resistojet. 

Cygnarowicz, T.A. ; Gibson, R.N., Jr. 

AIM Paper 67-662, Sept. 1967. 

Subsystems Analyses for a FURL Resistojet 

Control System. 

Eusanio, E.; Pisciotta, A., Jr. 

AIAA Paper 67-721, Sept. 1967. 

Perfonnance Tests of a 1/2-Hillipound 

(2.2 nW) Amnonia Resistojet Thrustor System. 

Ferguson, H.; Sovey, J.S. 

NASA TN D-4249, 1967. 

Low-Thrust Propulsion for the MORL. 

Goohn, H. 

J. Spacecr. Rockets, vol. 4, Feb. 1967, pp. 

183-187. 

01 :056: 1967 

01:057:1967 

01:058:1967 

01:059:1967 

01:060: 1967 

01:061:1968 

01:062:1968 

01:063:1968 

01:064:1968 

01:065:1968 

Auxiliary and Primary Electric Propulsion, 

Present and Future. 

Hickelsen, W.R. 

J. Spacecr. Rockets, vol. 4, Nov. 1967, pp. 

1409-1423. 

Electric Propulsion for Satellites. 

Hickelsen, W.R. 

Colorado State University. NASA CR-88064, 

1967. 

Ten-Ri 11 ipound Resistojet Performance. 

Page, R.J.; Short, R.A. 

AIAA Paper 67-664, Sept. 1967. 

Design, Development, Fabrication, Test, and 

Delivery of Electrothermal Engine Systems. 

Pugnire, T.K. 

Avco Corp. NASA CR-72362, 1967. 

Electrothermal Mi crothrust Systems. 

White, A.F. 

AIAA Paper 67-424, July 1967. 

Definition of a Resistojet Control System 

for the Manned Orbital Research Laboratory, 

Volune 4 - Ground and Flight Test Plan. 

Byke, R.M.; Greco, R.V.; Pisciotta, A., Jr. 

Douglas Aircraft Co., Inc. NASA CR-66603, 

1968. 

Definition of a Resistojet Control System 

for the Manned Orbital Research Laboratory, 

Volune 3 - Biouaste Utilization. 

Byke, R.M.; Greco, R.V.; Pisciotta, A., Jr. 

Douglas Aircraft Co., Inc. NASA CR-66602, 

1968. 

Resistojet Biouaste Utilization - Evaluation 

and System Selection. 

Byke, R.M.; Greco, R.V. 

AIM Paper 68-121, Jan. 1968. 

Definition and Performance of a Thermal 

Storage Resistojet. 

Cygnarowicz, T.A.; Gibson, R.N., Jr. 

AIM Paper 67-662, June 1968. 

Definition of a Resistojet Control System 

for the Manned Orbital Research Laboratory. 

Volune 2 - Resistojet Control System 

Anal ysi s . Eusanio, E.N.; Pisciotta, A., Jr. 

Douglas Aircraft Co., Inc. NASA CR-66601, 

1968. 

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01 :069: 1968 

01:070:1968 

01:071:1968 

01:072: 1968 

01:073:1968 

01:074: 1968 

01:075:1968 

Definition of a Resistojet Control System 

for the Manned Orbital Research Laboratory. 

Volune 1 - Surmary. 

Eusanio, E.N.; Pisciotta, A., Jr. 

Douglas Aircraft Co., Inc. 

1968. 

NASA CR-66600, 

Preliminary Tests of a Single-Axis Pmnonia 

Resistojet Attitude Control System. 

Ferguson, H.; Hunczak. H.R.; Sovey, J.S. 

NASA TM X-1677, 1968. 

Electric and Ion Propulsion. 

Forbes, S.G. 

In: Jet, Rocket, Nuclear, Ion and Electric 

Theory and Design, W.H.T. Loh, ed., 

Springer-Verlag, Inc., 1968, pp. 427-462. 

Definition of a Resistojet Control System 

for the Manned Orbital Research Laboratory. 

Volune 5 - Resistojet Design and 

Development. 

Greco, R.V.; Page, R.J.; Short, R.A. 

Douglas Aircraft Co., Inc. 

1968. 

NASA CR-66604, 

Definition of a Resistojet Control System 

for the Manned Orbital Research Laboratory. 

Greco, R.V.; Page, R.J.; Short, R.A. 

Douglas Aircraft Co., Inc. NASA CR-66604A, 

1968. 

Definition of a Resistojet Control System 

for the Manned Orbital Research Laboratory. 

Greco, R.V.; Page, R.J. 

Douglas Aircraft Co., Inc. NASA CR-129452, 

1968. 

Resistojet Control System Analysis - Definition of a Resistojet Control System for the 

Manned Orbital Research Laboratory. 

Halbach, C.R. 

NASA CR-66601, 1968. 

Electric Microthrusters Make It. 

Isley, W.C.; Mickelsen, W.R. 

Astronaut. Aeronaut.. June 1968, pp. 54-61. 

Optimal Control Application for Electrothermal Wltijet Systems on Synchronous 

Earth Spacecraft. 

Isley, W.C. 

AIM Paper 67-723, Dec. 1968. 

Auxiliary Electric Propulsion Status and 

Prospects. 

Isley, W.C.; Mickelsen, W.R. 

NASA TM X-61074, 1974. 

01:016:1968 

01 :077: 1968 

01:078:1968 

01:079:1968 

01:080: 1968 

01:081:1968 

01 :082: 1968 

01:083:1968 

01:084:1969 

01:085:1969 

01:086: 1969 

Attitude Control for Manned Space Stations. 

Kurzhals, P.R. 

AIAA Paper 68-1056, Oct. 1968. 

ATS-111 Resi stojet Thrustor System 

Performance. 

Lund, W.; Pugnire, T.K. 

AIM Paper 68-553, June 1968. 

Pmnonia Resistojet Engines. 

Marion, C.; Clorin, R. 

Presented at the International Colloquium on 

Satellite Attitude and Stabilization, Paris, 

May 28-31, 1968. 

Advanced Electric Propulsion Research. 

Semiannual Report, Dec. 31, 1967-June 30, 1968. 

Mickelsen, W.R. 

Colorado State University. NASA CR-96633, 

1968. 

Ten-Hi 11 ipound Resistojet Performance. 

Page, R.J.; Short, R.A. 

J. Spacecr. Rockets, vol. 5, July 1968, 

pp. 857-858. 

Definition of a Resistojet Control System for 

the Manned Orbital Research Laboratory. 

Page, R.J.; Short, R.A.; Greco, R.V. 

DAC-58134, vol. 5, Douglas Aircraft Co. NASA 

CR-66604, 1968. 

Subsystems Analysis for a MORL Resistojet 

Control System. 

Pisciotta, A., Jr. 

J. Spacecr. Rockets, vol. 5, Aug. 1968, 

pp. 948-954. 

Conception and Experimentation of an 

Electrothermal System of Orbital Propulsion. 

Thieck, J. 

IAF Paper P-175, International Astronautical 

Federation, Oct. 1968. 

Pmnonia Resistojet Station Keeping Subsystem 

Aboard Applications Technology Satellite/ 

ATSIIV. 

Callens, R.A. ; Pugnire, T.K.; Shaw, R. 

AIAA Paper 69-296, Mar. 1969. 

The Hybrid /Hydrazine/ Resistojet. 

Chapin, S.G. ; Pugnire, T.K. ; Schreib, R.R. 

AIAA Paper 69-496, June 1969. 

Resi stojet Systems Manned Spacecraft 

Appl ications. 

Charhut, D.E.; Greco, R.V. 

AIM Paper 69-255, Mar. 1969. 

1 
01:D87: 1969 

01:088: 1969 

01:089:1969 

01 :090: 1969 

01:091:1969 

01 :092: 1969 

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01:094:1969 

01:095:1970 

01 :096: 1970 

ATS-I11 Resistojet Thruster System 

Performance. 

Davis, W.S.; Lund, W.; Pugnire, T.K. 

J. Spacecr. Rockets, vol. 7, July 1969, 

pp. 790-794. 

Advance in the High Temperature Acceleration 

of Propellants. 

Ducati, A.C.; Giannini, G.H.; Huehlberger, E.; 

Todd, J.P. 

In: Proc. 3rd performance of High Tenperature 

Systems Conf., vol. 2, Gordon and Breach, 

Science Publishers, Inc. (New York), 1969, 

pp. 511-527. 

Achievement of Synchronous Orbit Using 

Electr i c Propul sion . Ghosh, R.; Hudson, G. 

AIAA Paper 69-275, Mar. 1969. 

Resistojet Control for Advanced Space 

Stations . Greco, R.V. 

Space/Aeronautics, vol. 51, Mar. 1969, 

pp. 82-84. 

Life Test of Six High Temperature 

Resi stojets. 

Halbach, C.R. ; Ownby, H.L. ; Page, R.J. ; 

Short, R.A. 

AIAA Paper 69-294, Mar. 1969. 

Pmnonia Resi stojet Thrustor. 

Marion, C.; Ckrin, R. 

DGLR Paper 69-016, Deutsche Gesellschaft fuer 

Luft- und Raumfahrt, May 1969. 

Pmnonia Resi stojet Stat ion-Keeping Subsystem 

Aboard Applications Technology Satel 1 i te 

Pugnire, T.K.; Shaw, R.; Callens, R. 

AIAA Paper 69-296, Mar. 1969. 

(ATS) -1V. 

ATS-I11 Resi stojet Thruster System 

Performance. 

Pugnire, T.K.; Davis, W.S. 

J. Spacecr. Rockets, vol. 6, no. 7, July 1969, 

pp. 790-794. 

Biowaste Resistojet System Definition for the 

NASA Space Station. 

Bliss, J.R.; Greco, R.V.; Nelson, W.G. 

AIM Paper 70-1132, Aug. 1970. 

El ectr i c Propu 1 si on by Res i stojets . Donovan, J.A.; Lord, W.T.; Savage, A. 

J. Br. Interplanet. SOC., vol. 23, Jan.,19 

pp. 65-77. 

70, 

01:097:1970 

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01:107:1970 

8 

Resistojet Waste ethane Utilization in 

Manned Space Application. 

Duncan, L.F.; Laubach, G.E. 

AIM Paper 70-1131, Sept. 1970. 

A Study of Resistojet Systems Directed to the 

Space Stat i on/Base . Duncan, L.F.; Proeschel, R.A.; Schaedle, O.C. 

North Pmerican Rockwell Corp. 

1970. 

NASA CR-111863, 

Resistojet Waste ethane Utilization in 

Manned Space Application. 

Duncan, L.F.; Laubach, G.E. 

AIM Paper 70-1 131, Aug. 1970. 

Proposals for Hydrazine and Pmnonia 

Resistojet Orbit and Attitude Control Systems 

for Satel 1 i tes. 

Earl, A.C. 

RAE-TR-70209, Royal Aircraft Establishment, 

Nov. 1970. 

Thermal and Material Considerations Pertinent 

to the Biouaste Resistojet. 

Enos, G.R.; Pugnire, T.K. 

AIM Paper 70-1135, Aug. 1970. 

Satellite Raising to Synchronous Orbit. 

J. Br. Interplanet. Soc., vol. 23, Oct. 1970, 

Free, B.A. I 

pp. 669-690. 

Advance Biouaste Electric Propulsion Systems. 

Goohan, H.; Yakut, H.H. 

J. Eng. Ind., vol. 92, Aug. 1970, pp. 613-620. 

Development of a Biowaste Resistojet. 

Halbach, C.R. ; Yoshida, R.Y. 

AIAA Paper 70-1133, Aug. 1970. 

Life Test Sumnary and High Vacuun Tests of 

lhlb Resistojets. 

Halbach, C.R.; Hill, C.S.; Yoshida, R.Y. 

J. Spacecr. Rockets, vol. 8, no. 4, Apr. 1970, 

pp. 414-416. 

Resistojet Thruster Life Tests and High 

Vacuun Performance. 

Halbach, C.R.; Hill, C.S.; Page, R.J.; 

Short, R.A.; Yoshida, R.Y. 

Marquardt Corp. NASA CR-66970, 1970. 

Electrothermal Thruster Performance with 

Biowaste Propellants. 

Krieve, W.F.; Hurch, C.K. 

AIAA Paper 70-1161, Sept. 1970. 
01:108:1970 

01 : 109: 1970 

01:110:1970 

01 : 1 1 1 : 1970 

01:112:1970 

01: 113: 1970 

01:114:1970 

01:115:1970 

01:116:1970 

01 : 117: 1970 

Two Stage (Resistojet/Ion Motor) Transfer of 

Camunications Satellites. 

Lord, W.T.; Parkinson, R.C. 

AIAA Paper 70-1116, Aug. 1970. 

El ect r i c Propul si on by Resi stojets . Lord, W.T.; Donovan, J.A.; Savage, A. 

J. Br. Interplanet. SOC., vol. 23, 1970, pp. 

65-77. 

Two-Stage (Resistojet/Ion Motor) Transfer of 

cammications Sate1 1 ites. 

Lord, W.T.; Parkinson, R.C. 

AIAA Paper 70-1116, Aug. 1970. 

The Use of Electric Hicrothrusters for Orbit 

Correction of Geostationary Satellites. 

Luquet, P. 

Automatic Control in Space 3, International 

Conference, 3rd. Toulouse, France, Mar. 2-6, 

1970; lnstrunent Society of America, 1970. 

Advanced Resistojet Propulsion and Control 

Systems for Spacecraft. 

Page, R.J.; Short, R.A. 

In: 

the 70's. American Society of Mechanical 

Engineers Space Technology and Heat Transfer 

Conference, Part 1, June 1970. 

Space Systems and Thermal Technology for 

Applied Resistojet Technology. 

Pugnire, T.K.; Shaw, R. 

AIM Paper 70-211, Jan. 1970. 

Thermal and Haterial Considerations Pertinent 

to the Biowast Resistojet. 

Pugmire, T.K.; Enos, G.R. 

AIM Paper 70-1135, Aug. 1970. 

Electronic Propulsion Systems for Long-Term 

Space Station Operations. 

Stuhlinger, E. 

In: Proc. Orbital International Laboratory 

and Space Sciences Conference, International 

Academy of Astronautics, 1969, pp. 464-482. 

Integrated Enviromntal Control/Life 

Support Resistojet Systems. 

VanLandingham, E.E.; Willis, S.P. 

AIAA Paper 70-1130, Aug. 1970. 

Integrated Envi romntal Control/Life 

Support Resistojet Systems. 

VanLandingham, E.E.; Willis, S.P. 

AIM Paper 70-1130, Sept. 1970. 

01 : 118: 1970 

01:119:1970 

01 : 120: 1971 

01: 121: 1971 

01:122:1971 

01:123:1971 

01:124:1971 

01: 125: 1971 

01: 126: 1971 

01 : 127: 1971 

Resistojet Thruster Life Tests and High 

Vacuun Performance. 

Yoshida, R.Y.; Halbach, C.R.; Page, R.J.; 

Short, R.A.; Hill, C.S. 

TK-S-974, Marquardt Corp. NASA CR-66970, 

1970. 

Life Test Sunnary and High Vacuun Tests of 

lOml b Resi stojets. 

Yoshida, R.Y.; Halbach, C.R.; Hill, C.S. 

AIAA Paper 70-1136, Apr. 1970. 

Biouaste Resistojet Propulsion System, 

Biological and Functional Analysis. Tasks 

1 and 2. 

Bionetics Corp. NASA CR-111977, Sept. 1971. 

Space Station (Modular) Hission Analysis. 

Volune 2, Appendix. 

HDC-2684-Vol-2, HcOonnel I-Douglas Astronautics 

Co. NASA CR-121078, 1971. 

Space Station (Modular) Hission Analysis. 

Vole 1, Hission Analysis. 

HDC-G2684-Vol-1, HcDonnell-Douglas 

Astronautics Co. NASA CR-121077, 1971. 

Resistojets Systems Studies Directed to the 

Space Station/Space Base. 

!he, 2.T.; GPPCO, R.V. 

HDC-G2125-Vol-2, HcDonnell -Douglas 

Astronautics Co. NASA CR-111880, 1971. 

Development of a Platinun-Thoriun Oxide Alloy 

for Resistojet Thruster Use. 

Albert, H.J.; Hill, J.S. 

Engel hard Hi neral s and Chemical s Corp. 

NASA CR-111959, 1971. 

Resistojet Systems Studies Directed to the 

Space Statiordspace Base. 

Bliss, J.R.; Greco, R.V. 

HDC-G2125-Vol-1, HcDonnell-Douglas 

Astronautics Co. NASA CR-111879, 1971. 

Design and Operational Characteristics of an 

Integrated Biowaste Resistojet System. 

Bliss, J.R.; Greco, R.V. 

AIM Paper 71-686, June 1971. 

Lon Thrust Propulsion Technology '71. 

Cohen, E.; Hurch, C.K. 

Proc. Int. Synp. on Space Technology and 

Science, Agne Publishing, Inc. (Tokyo), 1971, 

pp. 83-97. 

9 
01:128:1971 

01:129:1971 

01 : 130: 1971 

01: 131: 1971 

01:132:1971 

01: 133: 1971 

01:134:1971 

01:135:1971 

01:136:1971 

01: 137: 1971 

01 : 138: 1971 

Gasdynamics of Resistojets. 

Edwards, I.; Jansson, R.E.W. 

J. Br. Interplanet. SOC., vol. 24, Dec. 1971, 

pp. 729-742. 

Appl i ed Resi stojet Techno1 ogy . Enos, G.R.; Pugnire, T.K. ; Shaw, R. 

AIM Paper 70-211, Jan. 1971. 

A Canparative Study of Chemical and 

Nonchemical Propulsion Systems for Attitude 

Control and Orbit Correction of 

Geostationary Satellites in the 500 to 

1000-kg class. Part B: Application of the 

Propulsion Systems to a Particular Satellite 

Conf i gurat i on. 

Fraga, E.; Crespo, A. 

Instituto Nacional de Technica Aerospacial , ESRO-CR-38, July 1971. 

Chemical Nonequilibriun Effects in Biwaste 

Thruster Performance. 

Gaubatz, W.A.; James, N.E.; Page, R.J. 

AIAA Paper 71-688, 1971. 

Resistojet Systems Studies Directed to the 

Space Station/Space Base. 

Greco, R.V. 

McDonnell-buglas Astronautics Co. 

NASA CR-111878, 1971. 

Development of a Biwaste Resistojet. 

Halbach, C.R.; Yoshida, R.Y. 

J. Spacecr. Rockets, vol. 8, no. 3, Mar. 1971, 

pp. 213-277. 

Life Test Sunnary and High-Vacuun Tests of 

104illipound Resistojets. 

Halbach, C.R.; Hill, C.S.; Yoshida, R.Y. 

AIAA Paper 70-1133, Apr. 1971. 

10 mlb Biwaste Resistojet Performance. 

Halbach, C.R. 

AIM Paper 71-687, June 1971. 

Development of a Biwaste Resistojet. 

Halbach, C.R.; Yoshida, R.Y. 

J. Spacecr. Rockets, vol. 8, no. 3, Mar. 1971, 

pp. 273-277. 

krmonia Resistojet. Volune 1. 

Laville, M. 

French Space Technology, Information 

Propaganda Francaises, ed., Centre National 

d'Etudes Spatiales (Paris), 1971, pp. 387-392. 

Monopropellant Hydrazine Resistojet. 

Muenzer, F. B. 

Analysis Task Sumry Report, TRW Systems 

Group. NASA CR-122347, 1971. 

01: 139: 1971 

01:140:1971 

01:141:1971 

01:142:1971 

01:143:1971 

01: 144: 1971 

01:145:1972 

01: 146: 1972 

01:147:1972 

01:148:1972 

01: 149: 1972 

01 : 150: 1972 

An Experimental Investigation of Superheated 

Sub1 iming Sol id Thruster Performance. 

Owens, W.L., Jr. 

WSS/CI Paper 70-210, July 1971. 

Design of High-Performance Resistojets for 

Advanced Spacecraft . Page, R.J.; Short, R.A. 

AIM Paper 71-195, Jan. 1971. 

Performance of a 10 mlb Biwaste Resistojet. 

Phi 11 ips, D.G. 

SAE Paper 710769, Society of Autanotive 

Engineers, Sept. 1971. 

Electrothermal Hydrazine Engine Performance. 

Pugnire, T.K.; et al. 

AIAA Paper 71-760, June 1971. 

Appl ied Resi stojet Technology. 

Pugnire, T.K.; Shaw, R.; Enos, G.R. 

3. Spacecr. Rockets, vol. 8, no. 3, Mar. 1971, 

pp. 63-68. 

Life Test Sunnary and High Vacuun Tests of 

lOmlb Resi stojets. 

Yoshida, R.Y.; Halbach, C.R.; Hill, C.S. 

J. Spacecr. Rockets, vol. 8, no. 4, Apr. 1971, 

pp. 414-416. 

Biwaste Resistojet Propellant System 

Biological and Functional Analysis, Task 3. 

Bionetics Corp. NASA CR-111977-1, 1972. 

Definition of a Resistojet Control System for 

the Manned Orbital Research Laboratory. 

Douglas Aircraft Co., Inc. 

1972. 

NASA CR-130642, 

Space Station Executive Surmary. 

MDC-G2727, McDonnell-Douglas Astronautics Co. 

NASA CR-123719, 1972. 

Electrothermal Hydrazine Thruster Analysis 

and Performance Evaluation. 

Callens, R.A.; Murch, C.K. 

AIAA Paper 72-1152, Nov. 1972. 

Design Aspects of Resistojets for Satellite 

Attitude Control. 

Dixon, J.C.; Husgrove, P.J. 

J. Br. Interplanet. SOC., vol. 25, no. 10, 

Oct. 1972, pp. 585-595. 

Fabrication and Preliminary Testing of a 3 kw 

Hydrogen Resistojet. 

Donovan, J.A.; Lord, W.T.; Sherwood, P.J. 

AIM Paper 72-449, Apr. 1972. 

10 
01 : 151 : 1972 

01 : 152: 1972 

01:153:1972 

01: 154: 1972 

01: 155: 1972 

01: 156: 1972 

01 : 157: 1972 

01:158:1972 

01: 159: 1972 

01:160:1972 

Proposals for Hydrazine and Amnonia 

Resistojet Orbit and Attitude Control 

Systems for Sate1 1 i tes. 

Earl, A.G. 

J. Br. Interplanet. SOC., vol. 25, Jan. 1972, 

pp. 31-41. 

A Theoretical Study of the Performance of 

Resi stojet Nozzles. 

Edwards, I. 

Ph.D. Thesis, Southampton University, 

Sept. 1972. 

Energy Losses in Resistojet Nozzle Flows. 

Edwards, I.; Jansson, R.E.W. 

AIM Paper 72-455, Apr. 1972. 

mnopropellant Hydrazine Resistojet nodel 

Specification. 

Grabbi, R. 

TRW Systems Group. NASA CR-122377, 1972. 

Development of a Biaraste Resistojet 

Propulsion System Propellant Ranagement and 

Control Subsystem. 

Greco, R.V.; Bliss, J.R.; Wilkinson, H.C. 

AIAA Paper 72-448, Apr. 1972. 

Resistojet and Plasma Propulsion System 

Technology. 

Greco, R.V.; Bliss, J.R.; Rurch, C.K.; 

Clark, K.E.; Kelly, A.J. 

AIAA Paper 72-1124, 1972. 

Investigation of Bionaste Resistojets for 

Space Station Applications. 

Halbach, C.R. 

Advanced Rocket Technology. NASA CR-27123, 

1972. 

High Tenperature Biowaste Resistojets Using 

Electrically Conducting Ceramic Heaters. 

Halbach, C.R.; Page, R.J.; Short, R.A. 

AIAA Paper 72-454, Apr. 1972. 

Investigation of Biowaste Resistojets for 

Space Station Application. 

Halbach, C.R.; Page, R.J.; McCaughey, O.J.; 

Short, R. A. 

Advanced Rocket Technology. NASA CR-112159, 

1972. 

Evaluation of Advanced Conponent Concepts for 

an Integrated Environmental Control/Life 

Support Resistojet Control System. 

Halbach, C.R.; Arthur, P.D.; Page, R.J. 

Advanced Rocket Technology. NASA CR-112104, 

1972. 

01:161:1972 

01:162:1972 

01:163:1972 

01 : 164: 1972 

01 : 165: 1972 

01: 166: 1972 

01:167:1972 

01 : 168: 1972 

01 : 169: 1972 

01: 170: 1972 

Investigation of Biowaste Resistojets for 

Space Station Applications. 

Halbach, C.R. 

Advanced Rocket Technology. NASA CR-172674, 

1972. 

System Study of Electric Propulsion for 

Rilitary Space Vehicles. 

Hawk, C.; Baty, R.; Rosen, S.; Quirk, J. 

AIAA Paper 72-493, Apr. 1972. 

Viscous Effects on Biowaste Resistojet Nozzle 

Performance. 

Kallis, J.R.; Gooctnan, H.; Halbach, C.R. 

J. Spacecr. Rockets, vol. 9, no. 12, 

Dec. 1972, pp. 869-875. 

Hydrogen Resistojets for Primary Propulsion 

of Camunications Satellites. 

Lord, W.T.; Parkinson, R.C.; Allen, K.; 

Donovan, J.A.; Sherwood, P.J. 

RPE-TM-605, Rocket Propulsion Establishment, 

July 1972. 

A Suggestion for a Versatile Electric 

Thruster Carprising Resistojets and Ion 

mors. 

Lord, W.T. 

RPE-TR-71-5, Rocket Propulsion Establ istunent, 

Dec. 1972. 

El ect rot hem1 Hydrazi ne Thruster 

Devel opment . Rurch, C.K.; Hunter, C.R. 

AIM Paper 72-451, Apr. 1972. 

Ronopropel lant Hydrazine Resistojet 

Prel imi nary Design Task. 

Murch, C.K. 

TRW Systems Group. NASA CR-122376, Feb. 1972. 

Technology Development and Demonstration of a 

Low Thrust Resistojet Thruster. 

Pfeifer, G.R. 

Rarquardt Carpany. NASA CR-112160, 1972. 

Technology Development of a Biowaste 

Resistojet. Volw 1. 

Phillips, D.G. 

Rarquardt Corp. NASA CR-112149, 1972. 

Technology Development of a Biowaste 

Resistojet. Volw 2. 

Phillips, D.G. 

NASA CR-112150, 1972. 

11 
01:171:1972 

01 : 172: 1972 

01 : 173: 1973 

01: 174: 1973 

01:175:1973 

01:176:1973 

01:177:1973 

01:178:1973 

01 : 179: 19 73 

01 : 180: 1973 

01: 181: 1973 

Progressive Attitude and Orbit Correction 

with the Aid of Hydrazine - Propulsion 

Systems and Their Employment in Europe. 

Schmitz, H.; Midneck, H. 

DGLR Paper 72-078, Deutsche Gesellschaft fuer 

Luft- und Raunfahrt, Oct. 1972. 

Construction of a High-Performance Resistojet 

for Satellite Propulsion. 

Sherwood, P.J. 

J. Br. Interplanet. SOC., vol. 25, Oct. 1972, 

pp. 573-583. 

Development of a Biwaste Resistojet 

Propulsion System. 

HcDonnell-Douglas Astronautics Co. NASA 

CR-132269, July 1973. 

Electric Propulsion of Space Vehicles. 

In: 

Vehicles, Institution of Electrical Engineers, 

1973. 

Proc. Electric Propulsion of Space 

The Electric Propulsion of Space Vehicles. 

Bright, A.W.; Hakin, B. 

Contenp. Phys., vol. 14, Jan. 1973, pp. 25-38. 

Monopropellant Thruster Performance 

Augnentation Heater Development Program. 

Bruun, E.R. ; Kingsley, T.C. 

AFRPL-TR-80-73, Air Force Rocket Propulsion 

Laboratory, Feb. 1981. 

Performance Testing of a 3 kW Hydrogen 

Resistojet. 

Donovan, J.A.; Lord, W.T. 

Paper RPE-TN-237, Rocket Propulsion 

Establishent, Hay 1973. 

Current Technology in Ion and Electrothermal 

Propul si on. 

Finke, R.C.; Hurch, C.K. 

AIM Paper 73-1253, Nov. 1973. 

Analysis of Near-Earth Hissions Using Mixed 

Electric Thruster Tug. 

Holdaway, R.; Jansson, R.E.W. 

In: 

Space Vehicles, Institution of Electrical 

Engineers (England), 1973, pp. 233-237. 

Proc. Conf. on Electric Propulsion of 

Study of Monopropellants for Electrothermal 

Thrusters: Analytical Task Summry Report. 

Kuenzly, J.D.; Grabbi, R. 

TRW Systems Group. NASA CR-132921, 1973. 

Electric Propulsion Status and Development 

Plans - NASA Programs - Primary and Auxiliary 

Systems. 

Lazar, J. 

AIAA Paper 73-1143, Oct. 1973. 

01: 182: 1973 

01: 183: 1973 

01:184:1973 

01:185:1973 

01:186:1974 

01:187:1974 

01:188:1974 

01:189:1974 

01:190:1974 

01:191:1974 

01 : 192: 1974 

12 

Optimisation of Performance of Small 

Electrotheml Thrusters Using Polyatanic 

Propellants. 

Leuin, R. ; Edwards, I. ;Jansson. R.E.W. 

In: 

Space Vehicles, Institution of Electrical 

Engineers (England), 1973, pp. 161-165. 

Proc. Conf. on Electric Propulsion of 

Monopropellant Hydrazine Resistojet: F1 ight 

Application Design. 

Hurch, C.K. 

TRW Systems Group. NASA CR-132763, 1973. 

Monopropellant Hydrazine Resistojet: Data 

Correlation. 

Hurch, C.K. 

TRW Systems Group. NASA CR-130762, 1973. 

The Design and Application of Hybrid 

Hydrazine Resistojets. 

Stott, 0.; Richardson, N.K. 

In: 

Space Vehicles, Institution of Electrical 

Engineers (England), 1973, pp. 156-160. 

Proc. Conf. on Electric Propulsion of 

Survey of Electric Propulsion Capability. 

Clark, K.E. 

AIAA Paper 74-1082, Oct. 1974. 

Resistojet Testing at the Rocket Propulsion 

Establishment. 

Donovan, J.A. 

RPE-TR-74 TR-24, Rocket Propulsion 

Establishment, Feb. 1974. 

Electric Propulsion in the UK. 

Fearn, D.G. 

DGLR - Fachbuchreihe, vol. 5, 1974, pp. 22-30. 

Theoretical Performance of Pmnonia, Hydrogen, 

and Biwaste Resistojets. 

Jansson, R.E.W.; Edwards, I. 

J. Br. Interplanet. SOC., vol. 27, June 1974, 

pp. 433-442. 

Study of Monopropellants for Electrothermal 

Thrusters. 

Kuenzly, J.D. 

TRW Systems Group. NASA CR-144683, 1974. 

Study of Monopropellants for Electrothermal 

Thrusters: Design and Fabrication Task 

Summry Report. 

Kuenzly, J.D. 

TRW Systems Group. NASA CR-139017, 1974. 

Study of Monopropellants for Electrothermal 

Thrusters. Evaluation Test Program Task 

Summry Report. 

Kuenzl y , J . D. 

TRW Systems Group. NASA CR-139072, 1973. 
01 : 193: 1974 

01:194:1974 

01: 195: 1974 

01: 196: 1974 

01:197:1974 

01:198:1974 

01: 199: 1975 

01:200: 1975 

01:201:1975 

A Short Survey of RPE Work on Electric 

Propulsion by Resistojets. 

Lord, W.T. 

RPE-TR-19, Rocket Propulsion Establishment, 

Feb. 1974. 

Electrothermal Hydrazine Thruster Development 

for Lar-Thrust Applications. 

Murch, C.K. 

In: Properties of Hydrazine and Its 

Applications as an Energy Source; Proc. Int. 

Conf., Centre National d'Etudes Spatiales 

(Paris), 1974, pp. 341-349. 

Elect-Thermal Hydrazine Reactor 

Development. 

Pugnire, T.K.; Davis, W. 

In: JA"AF Propulsion Meeting, 1973, vol. 3, 

Addendum, Jan. 1974, pp. 17-22. (Also NASA 

CR-136739, 1974.) 

Performance and Space Application Potentials 

of Electrothermal Reactors - Hydrazine 

Engi nes . Pugnire, T.K. 

In: Properties of Hydrazine and Its 

Applications as an Energy Source; Proc. Int. 

Conf., Centre National d'Etudes Spatiales 

(Paris), 1974, pp. 351-371. 

The Electrothermal Hydrazine Reactor. 

Stott, D. 

IAF Paper 74-132, International Astronautical 

Federation, Sept. 1974. 

Electric Propulsion - Past History and Future 

Prospects. 

Stuhlinger, E. 

AIM Paper 74-1081, Oct. 1974. 

Survey of Electric Propulsion Capability. 

Clark, K.E. 

J. Spacecr. Rockets, vol. 12, no. 11, Nov 

1975, p. 641. 

A Survey of Electric Propulsion Research and 

Development in the UK - European Thrustors 

for N-S Stationkeeping of Synchronous 

Satel 1 i tes. 

Fearn, D.G. 

RAE-TR-75053, Royal Aircraft Establishment, 

June 1975. 

Feasibility Demonstration of a 5 lb Thrust 

Non-Catal yti c Electrothermal Hydrazine 

Thruster. 

O'Connor, T.J.; Davis, W.S. 

AFRPL-TR-75-43. AUg. 1975. 

01 :202: 1975 

01:203: 1975 

01 :204: 1975 

01:205:1975 

01 :206: 1976 

01:207:1976 

01 :208: 1917 

01:209: 1977 

01:210: 1977 

01:211: 1977 

13 

Cost Optimization of a Re-Supplied 

Cormunications Satellite System with 

Mixed-Thruster Electric Propulsion. 

Parkinson, R.C. 

J. Br. Interplanet. SOC., vol. 28, Jan. 1975, 

pp. 26-37. 

Electrothermal Hydrazine Reactors. 

Pugnire, T.K. 

AIM Paper 75-1244, Sept. 1975. 

State of Development and Application of 

Catalytic and Electrothermal Hydrazine 

Propulsion Units for Trajectory and Attitude 

Control of Satel 1 i tes. 

Schmitz, H.D. 

RAE-LIB-TRANS-1865, Royal Aircraft 

Establishment, Nov. 1975. 

Investigation on an Electrothermal Hydrazine 

Thruster. 

Twardy, H. 

IAF Paper 75-036, International Astronautical 

Federation, Sept. 1975. 

High Performance Electrothermal Hydrazine 

Thruster /HiPEHT/ Development. 

Grabbi, R.; Murch, C.K. 

AIM Paper 76-656, July 1976. 

Noncatalytic Hydrazine Thruster Developnent - 

0.050 to 5.0 Pounds Thrust. 

Hurch, C.K.; Sackheim, R.L.; Kuenzly, J.D.; 

Callens, R.A. 

AIAA Paper 76-658, July 1976. 

Flcu-Field CaFputation in the Heater and 

Nozzle of a Power Augnented Electrothermal 

Hydrazine Thruster. 

Barber, B.C. 

In: ESA Attitude and Orbit Control Systems, 

NOV. 1977, pp. 461-470. 

Elect-Thermal Hydrazine Thruster 

Visualization Study. 

Barter, A.J. 

In: ESA Attitude and Orbit Control Systems, 

NOV. 1977, pp. 471-477. 

Development of a Power Augnented 

Electrothermal Hydrazine Thruster. 

Keyte, G.E. 

In: ESA Attitude and Orbit Control Systems, 

NOV. 1977, pp. 453-459. 

Electrothermal, Noncatalytic Hydrazine 

Engine. 

O'Connor, T.J.; Davis, W.S.; Pugnire, T.K. 

In: The 1976 JANNAF Propulsion Meeting - vol. 4. CPIA-WBL-280, Chemical Propulsion 

Information Agency, 1977, pp. 305-320. 

-1 

i 

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01:213:1978 

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01:216:1979 

01:217:1979 

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01:219:1979 

01:220:1980 

01:221:1980 

Flight Applications of High Performance 

Electrothermal Thrusters. 

Zafran, S.; Murch, C.K.; Grabbi, R. 

AIM Paper 77-965, July 1977. 

Performance Prediction of Power Augnented 

Electrothermal -Hydrazi ne Thrusters. 

Hayn, D.; Braitinger, M.; Sct-unucker, R.H. 

AIAA Paper 78-1064, July 1978. 

Applications of Power Augnented Hydrazine 

Thrusters. 

Pugnire, T.K.; Mack1 is, H. ; Sackheim, R.L. 

AIAA Paper 78-1065, July 1978. 

Construction of a High Performance Resistojet 

for Satellite Propulsion. 

She&, P.J. 

PERME-TR-99, Propellants, Explosives, and 

Rocket Motor Establishment, Nov. 1978. 

Electrothermal Hydrazine Thruster. 

ESA-CR(P)-1466, British Aerospace Dynamics 

Group, 1979. 

Hydrazine Electrothermally Augnented Thruster 

(HEAT). 

Finston, R.; Meese, R.A. 

AIAA Paper 79-1332, June 1979. 

The Next Generation of Spacecraft Orbit 

Control Propulsion Systems. 

Sackheim, R.L.; Fritz, O.E.; Macklis, H. 

AIM Paper 79-1301, June 1979. 

Technical Development Problems of 

Electrothermal Hydrazine Thrusters. 

Valentini, R.; Lecoq, fl.; Maqueet, J. 

In: Space, Space Telecomnunications and 

Sate1 1 ite Radio Broadcasting: 

the Next Decade; Int. Conf., Centre National 

d'Etudes Spatiales (Toulouse), 1979, pp. 

Objectives for 

519-526. 

Monopropellant Thruster Performance 

Augmentat ion Heater Development Program. 

Bruun, E.R. 

In: The 1980 JA"AF Propulsion Meeting - 

VO~. 4. 1980, pp. 97-124. 

Flight Design of an Electrothermal Hydrazine 

Thruster. 

Kuenzly, J.D. ; Carlson, R.A. ; Sackheim, R.L. ; 

Rudey, C. 

In: The 1980 JANNAF Propulsion Meeting - vol. 4. 1980, pp. 49-96. 

01 :222: 1980 

01:223:1980 

01:224:1981 

01:225: 1981 

01:226:1981 

01:227:1981 

01:228:1981 

01:229:1981 

01:230:1982 

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01 :232: 1982 

Long Life Electrothermal Thruster 

Development . Kuenzly, J.D. 

AFRPL-TR-80-3, TRW Defense and Space Systems 

Group, May 1980. 

Inproved Performance Monopropel lants (WF-9) 

Electrothermal Thruster Feasibi 1 ity. 

Rendleman, J.D.; Lester, J.T. 

AFRPL-TR-80-4, Air Force Rocket Propulsion 

Laboratory., Aug. 1980. 

Monopropellant Thruster Performance 

Augnentation Heater Development Program. 

Brunn, E.R.; and Kingsley, T.C. 

AFRPL-TR-80-73, Feb. 1981. 

Flight Qualification of the Augnented 

Electrothermal Hydrazine Thruster. 

Dressler, G.A.; Morningstar, R.E.; 

Sackheim, R.L.; Fritz, D. 

AIAA Paper 81-1410, July 1981. 

A Review of Future Orbit Transfer Technology 

for Space Industrialization. 

Fearn, D.G. 

RAE-TR-81080 and RAE-SPACE-599, Royal Aircraft 

Establishment, June 1981. 

Flight Qualification of the Augnented 

Hydrazine Thruster. 

Saltz, L.E.; Emnons, D.L. 

In APL. The 1981 JA"AF Propulsion Meeting, 

VO~. 6, flay 1981, pp. 465-477. 

Augnented Electrothermal Hydrazine Thruster 

(AEHT) Development. 

Schmitz, H.D.; Steenborg, M. 

AIM Paper 81-1409, July 1981. 

Electrothermal Hydrazine Thruster. 

Taylor, C.B. 

BAE-RPT/EHT/40212-VOL-l, British Aerospace 

Dynamics Group, 1981. 

Electric Propulsion Research and Technology 

in the United States. 

Hudson, W.R.; Vondra, R.J.; Cochran, T.; 

Pawlick, E. 

AIAA Paper 82-1867, Nov. 1982. 

Resistojet Propulsion for Large Spacecraft 

Mirtich, fl. J. 

NASA TM-83489, 1982. 

Systems. 

The Design and Technology Development for a 

150 mlb Resistojet for H2 or "3. 

Page, R.J.; Stoner, W.A. 

AIM Paper 82-1949, Nov. 1982. 

14 
01:233: 1982 

01:234: 1983 

01:235: 1983 

01:236: 1983 

01237: 1983 

Electrothermal Decarposition of 

Nonanethyl hydrazi ne. 

Schitz, H.D.; Tiedtke, P. 

In: Research and Developnent: Technical and 

Scientific Publications 1982, Forschung und 

Entwicklung, 1982, pp. 255-260. 

Design and Development Approach for the 

Augnented Catalytic Thruster (ACT). 

RcKevitt, F.X. 

AIM Paper 83-1255, June 1983. 

Considerations on Technologies and Missions 

for Non-Chemical Propulsion. 

Nolitor, J.H. 

IAF Paper 83-400, International Astronautical 

Federation, Oct. 1983. 

Augnented Electrothermal Hydrazine Thruster 

Development. 

Schmitz, H.D.; Steenborg, R. 

J. Spacecr. Rockets, vol. 20, Rr.-Apr. 1983, 

pp. 178-181. 

Electrothermal Thruster Diagnostics. 

Volune 2 - Technical. 

Zafran, S.; Jackson, B. 

TRW, Inc. NASA CR-168174-Vol-2, 1983. 

01:238: 1983 Electrothermal Thruster Diagnostics. 

Volune 1 - Executive Sunnary. 

Zafran, 5.; Jackson, 8. 

TRW, Inc. NASA CR-168174-Vol-1, 1983. 

01239: 1984 The NASA Electric Propulsion Program. 

Byers, D. 

17th International Electric Propulsion 

Conference, IEPC 84-01, 1984. 

01:240: 1984 Space Station Propulsion Analysis Study. 

Donovan, R.R.; Sovey, J.S.; Hannun, N.B. 

AIAA-84-1326, 1984. 

01:241: 1984 Design, Performance, and Operational Scaling 

Criteria for Electrically Augnented 

Hydrazine Thrusters. 

McKevitt, F.X.; Schwam, F.R. 

AIM Paper 84-1234, June 1984. 

01 :242: 1984 Radiative Resistojet Performance Characterization Tests. 

Riyake, C.I. 

NASA CR-174763, 1984. 

15 
02:001:1929 

02:002:1933 

02:003:1949 

02:004:1951 

02:005:1953 

02:006:1956 

02:007:1956 

02:008: 1957 

02:009: 1959 

02:010:1959 

02:011:1959 

Category 2 - Arcjets 

The Cathode Drop in an Electric Eye Arc. 

Mackeonn, S.S. 

Phys. Rev., vol. 34, 1929, pp. 611-614. 

Swirling Flows in Tubes and Their Application 

in the Stabilization of Electric Arcs. 

Traub, E. 

Ann. Physik (Leipzig), vol. 18, no. 169, 1933. 

The Vaporization of the Cathode in the 

Electric Arc. 

Holm, R. 

J. Appl. Phys., vol. 20, July, 1949, p. 715. 

Boride Cathodes. 

Lafferty, J.M. 

J. Appl. Phys., vol. 22. no. 3, Mar. 1951, 

p. 299. 

The Energy Balance Equation for the Positive 

Colums of High Pressure Arcs. 

Champion, K.S.W. 

University of Birmingham, Proc. Phys. SOC., 

vol. 866, 1953, p. 169. 

Elektrische Bogen und Thennisches Plasma. 

Finkelnberg, W.; Maecker, H. 

Handbuch der Physi k, Ed. XXII, Springer-Verlag 

(Berlin), 1956, pp. 254-444. 

Thermionic Emission, Field Emission, and the 

Transition Region. 

Murphy, E.L.; Good, R.H., Jr. 

Phys. Rev., vol. 102, 1956, pp. 1464-1473. 

Excitation Theory of Arcs with Evaporating 

Cat h&s . Von Engel, A.; Robson, A.E. 

Proc. Roy. SOC., vol. A242, 1957, pp. 217-236. 

Plasma Propulsion. 

Cann, G.L.; Ducati, A.C. 

ARS Preprint 59-1010, American Rocket Society, 

1959. 

Carparison of Propulsion Systems: Solar 

Heating, Arc Thermodynamics, and Arc Magnet* 

hydrodynani cs. 

Ehricke, K.A. 

Proc. Advanced Propulsion Systems Syrrposium, 

Pergamon Press, 1959, p. 71. 

The Plasma Jet as an Electric Propulsion 

System for Space Application. 

Heller, G.B. 

ARS Preprint 1040-59, American Rocket Society, 

Nov. 1959. 

02:012: 1959 

02:013:1959 

02:014: 1959 

02:015:1960 

02:016: 1960 

02:017:1960 

02:018:1961 

02:019:1961 

02:020:1961 

02:021:1961 

02:022: 1961 

16 

Emission bchanism of Cold cathode Arcs. 

Hernquist, K.G. 

Phys. Rev., vol. 109, 1958, pp. 636-646. 

T-F Theory of Electrode Emission in High 

Current Arcs. 

Lee, T.H. 

J. Appl. Phys., vol. 30, 1959, pp. 166-171. 

The Electric Arc. 

Sanervi 1 le, J . M. 

John Wiley, New York, 1959, p. 64. 

Energy Distribution and Cooling Effect of 

Electrons Emitted fran an Arc Cathode. 

Lee, T.H. 

J. Appl. Phys., VO~. 31, 1960, pp. 924-927. 

Arc Plasma Thrustor Studies. 

Page, R.J., et al. 

ARS Preprint 1505-60, American Rocket Society, 

Dec. 1960. 

Arc Plasma Thrustor Studies. 

Page, R.J.; Buhler, R.D.; Stoner, W.A.; 

Masser, P.S. 

ARS Preprint 1508-60, American Rocket Society, 

1960. 

Arc Jet Application Study. 

General Electric Co. NASA CR-140076, 1961 

Electrode Cmponents of the Arc Discharge. 

Ecker, G. 

Ergeb. Exakt. Naturwiss 33, 1-104, 1961. 

Study of Arc Jet Propulsion. 

Gerhard, H. 

ARS Paper 174861, American Rocket Society, 

1961. 

Arc Jet Engine Performance - Experiment and 

Theory, 111. 

John, R.R., Chen, M.M.; Connors, J.F.; 

Hoercher, H.E. 

ARS Preprint 2135-61, American Rocket Society, 

Oct. 1961. 

Arc Jet Engine Performance - Experiment and 

Theory, 11. 

John, J.R.; Mironer, A.; Macomber, H.; 

Connors, J.F. 

IAS/ARS Joint Meeting Preprint 61-101-1795, 

June 1961. 
02023: 1961 

02:024:1961 

02:025:1961 

02:026: 1961 

02:027:1961 

02:028:1961 

02:029: 1961 

02:030: 1962 

02:031: 1962 

02 : 032: 1962 

02:033: 1962 

02 : 034 : 1962 

Recent Advances in Electric Arc Plasma 

Generation Technology. 

John, R.R.; Bade, W.L. 

ARS J., vol. 31, no. 1, Jan. 1961, pp. 4-117. 

Dynamics of Arc Jet Systems. 

Martinek, F.; Vaughn, G.F.; GeideMn, W.A. 

ARS Preprint 61-98-1792, American Rocket 

Society, June 1961. 

Recent Experimental Plasmajet Thrustor 

Results. 

Hasser, P.S. 

ARS Preprint 61-100-1794, American Rocket 

Society, June 1961. 

Recent Advances in High Pressure, High Parer 

Arcs. 

Reid, J.W. 

ARS Preprint 61-2127, American Rocket Society, 

Oct. 1961. 

Resistance Heating in the Arc Cathode Spot 

Zone. 

Rich, J.A. 

J. Appl. Phys., vol. 32, 1961, pp. 1023-1031. 

Performance Characteristics of the 3OOO Cycle 

Electrothermal Rocket. 

Spongberg, R.H. 

ARS Preprint 61-99-1793, American Rocket 

Society, June 1961. 

Developnent of a Thermal Vacuun Engine. 

Stoner, W.A.; Masser, P.S. 

Plasmadyne Corp. ASD-TR-61-243, June 1961. 

Developnent of a Thermal Arc Engine. 

Gianni ni Scient i f i c Corp. ASD-TDR-62-749, 

July 1962. 

Development of a Thermal Arc Engine. 

Plasmadyne Corp. APL-TOR-64-55, Hay, 1964. 

The Developnent of an Elect-Thermal 

Propulsion System. 

Plasmadyne Corp. NASA CR-125663, 1961. 

Theoretical and Experimental Research on 

Thermal Arcjets. 

Avco Corp. ASD-TDR-62-616, Aug. 1962. 

Effect of Nonequilibriun Flow in Thermal 

Arc-Jet Engines. 

Chen, H.H. 

RAD-TR-62-25, Avco Corp. 

16071, Sept. 1962. 

(NASA contract NAS8- 

02:035: 1962 

02:036:1962 

02:037:1962 

02:038:1962 

02 : 039 : 1962 

02:040:1962 

02:041:1962 

02:042: 1962 

02 : 043 : 1962 

02 : 044 : 1962 

Parer Plant Considerations for an Arcjet 

Space Propulsion System. 

Chen, H.H.; Connors, J.F.; John, R.R. 

Space Power Conference, Santa fbnica, CA, 

Sept. 25-28, 1962, American Rocket Society. 

Sept. 1962. 

Materials Problems Related to Electric Arc 

Jets. 

Gates, D.W.; HcKenna, Q.H. 

ARS Preprint 2353-62, American Rocket Society, 

Mar. 1962. 

Materials Requirements for Plasma Propulsion. 

Gates, D.W. 

Prentice Hall, 1962, p. 123. 

Electric Arcs and Thermal Plasmas. 

Finkelnberg, W. and Haecker, H. 

In: Handbook of Physics - vol. 12. 

Springer-Verlag (Berlin), 1956, pp. 254-444. 

Research and Developnent of a 1-kU Plasmajet 

Thrustor. 

Greco, R.V.; Stoner, W. 

ARS Preprint 2350-62, American Rocket Society, 

Mar. 1962. 

Arc Jet Engine Performance - Experiment and 

John, R.R.; Chen, H.H.; Connors, J.F.; 

Hegrue, J. 

ARS Preprint 2345-62, American Rocket Society, 

Mar. 1962. 

TheGry, E. 

Arc Jet Engine Performance - Experiment and 

Theory, V. 

John, R.R., et al. 

ARS Preprint 62-2667, American Rocket Society, 

Nov. 1962. 

Properties of Plasma as They Pertain to TAJ 

(Thermal Arc Jet) and JxB (WID WCT) Devices. 

Kerr, G.P.; Free, B.A. 

ASD-TDR-62-887, Oct. 1962. 

Magnetically Diffused Radial Electric Arc Air 

Heater Employing Water Cooled Copper 

E 1 ectrodes . Mayo, R.F.; Davis, D.D. 

ARS Preprint 62-2453, American Rocket Society, 

Mar. 1962. 

Spatial Nonuniformity Effects in 

Elect rot hermal Propul si on. 

Hironer, A.; Hacomber, H. 

ARS J., ~01. 32, 1962, pp. 1412-1413. 

17 
02 : 045 : 1962 

02:046:1962 

02:047:1962 

02:048:1962 

02:049:1962 

02:050:1962 

02:051:1962 

02:052:1963 

02:053:1963 

02:054:1963 

Experiments on Electric Propulsion by mans 

of Electrothermal Engines. 

Robotti, A.C.; Oggero, H.V. 

In: 

Press, 1962, pp. 299-313. 

High Tenperature in Aeronautics, Pergmn 

Anode Losses in Argon Arcs and Their 

Reduction by Transpiration Cooling. 

Schoeck, P.A.; Eckert, E.R.G.; Wutzke, S.A. 

ARL-62-341, Aeronautical Research 

Laboratories, Apr. 1962. 

Sunnary of Pub1 ished Literature Concerned 

with Electric Arc Phenanena Pertinent to 

Plasma Jet Devices. 

Skifstad, J.G. 

TH-62-4, Purdue University, Aug. 1962. 

Electrode Development for 30 kW 

Electrothermal Arc Jet Engine. 

Spisz, E.W. 

NASA CR-82607, Hay 1962. 

Theoretical Enthalpy Distribution of Air in 

Steady Flow Along the Axis of a Direct 

Current Electric Arc. 

Stine, H.A.; Watson, V.R. 

NASA TN D-1331, 1962. 

Development of a Thermal Arc Engine. 

Tod, J.P. 

Gi anni ni Scienti f i c Corp. 

July 1962. 

ASD-TDF-62-749, 

Feasi bi 1 i ty of Arcjet-Propel led Spacecraft. 

Yarpvych, H.; deweiss, F.A.; John, R.R. 

Astronaut., vol. 7, no. 6, June 1962, 

pp. 36-42. 

Theoretical and Experimental Investigation of 

Arc Plasma-Generation Technology. Part 2, 

Volune 1: A Theoretical and Experimental 

Study of Thermionic Arc Cathodes, 

Bade, W.L.; Yos, J.H. 

Avco Corp. ASD-TR-62-729, Sept. 1963. 

A Chemical Arcjet Rocket Feasibi 1 i ty Study. 

Bender, R.W. 

In: Electric Propulsion Development, Progress 

in Astronautics and Aeronautics, vol. 9, 

Academic Press 1963, pp. 95-120. 

Theoretical and Experimental Investigation 

of Arc Jet Engine Nozzle Flow. 

Bennett, S. 

Avco Corp. NASA CR-55753, 1963. 

02:055: 1963 

02:056:1963 

02:057:1963 

02:058: 1963 

02:059:1963 

02:060:1963 

02:061: 1963 

02:062:1963 

02:063:1963 

02:064:1963 

18 

Thermal Arc Jet Research. 

Cann, G.L.; Moore, R.A.; Buhler, R.D.; 

Harlotte, G.L. 

Electro-Opti cal Systems, Inc. ASD-TDR-63-632, 

Aug. 1963. 

Experimental Evaluation of a Direct Current 

Lou-Pressure Plasma Source. 

hitz, S. 

NASA TN 0-1659, 1963. 

Cryogenic Propellant Feed Systems for 

Electrothermal Engines. 

Fowle, A.A. 

Arthur D. Little, Inc. CR-64470, Jan 1963. 

Research and Development of a 1-kU Plasmajet 

Thruster. 

Greco, R.V.; Stoner, W.A. 

AIM J., ~01. 1, 1963, pp. 320-324. 

Instabi 1 i ty of Arc Col ms. 

Harvey, J.K.; Sinpkins, P.G.; Adcock, B.D. 

AIAA J., vol. 1, 1963, p. 714. 

Objectives and Design of a 1-kU Arcjet 

Engine for Space Flight Testing. 

Humpel, H.; Page, R.J. 

In: 

Aeronautics, vol. 9, Academic Press, 1963, 

p. 3. 

Development Progress in Astronautics and 

Possible Effects of Nonuniform Flows on 

Performance of Electrothermal Thrusters. 

Jack, J.R.; Schaefer, J.W. 

NASA TN D-1732, 1963. 

Arc Jet Engine Performance, Experiment and 

Theory. 

John, R.R.; Bennett, S.; Connors, J.F. 

AIM J., VO~. 1, 1963, pp. 2517-2525. 

Theoretical and Experimental Investigation of 

Arc Plasma-Generation Technology. Part 2, 

Volune 2: Arc Colm Theory, Electrode 

Haterials Behavior, and Hagnetic Field Arc 

Discharge Interact ion, 

John, R.R.; Bade, W.L.; Chen, H.H.; 

Debolt, H.; Gibbs, T.W.; Hoercher, H.; 

Lieberrnann, R.; Neurath, P.; Yos, J.H. 

Avco Corp. ASD-TR-62- 729, Sept. 1963. 

Theoretical and Experimental Investigation of 

Arc Plasma-Generation Technology. Part 1: 

Applied Research on Direct and A1 ternati ng 

Current Electric Arc Plasma Generators. 

John, R.R.; Debolt, H.; Hermann, H.; 

Hogan, W.; Kusko, A.; Liebermann, R. 

Avco Corp. ASD-TR-62-729, Sept. 1963. 
02:065:1963 

02:066: 1963 

02:067:1963 

02:068:1963 

02:069:1963 

02:070:1963 

02:071:1963 

02:072:1963 

02:073: 1963 

02:074: 1963 

Arc Jet Engine Performance - Experiment and 

Theory, IV. 

John, R.R.; Chen, M.H.; Connors, J.F.; 

Hegrue, J.F. 

In: Electric Propulsion Development Progress 

in Astronautics and Aeronautics, vol. 9, 

Academic Press, 1963, pp. 43-68. 

Thirty-Day Endurance Test of a 30 kw Arc Jet 

Engine. 

John, R.R.; Connors, J.F.; Bennett, S. 

AIM Paper 63-274, 1963. 

Thermal Arc Jet Research. 

John, R.R.; Bennett, S.; Connors, J.F.; 

Enos, G. 

Avco Corp. ASD-TOR-63-7 17, June 1963. 

Energy Addition and Loss tkchanisms in the 

Thermal Arc Jet Engine. 

John, R.R.; et al. 

AIAA Paper 63-022, 1963. 

Thirty Ki louatt Plasmajet Rocket-Engine 

Development. 

John, R.R.; et al. 

Avco Corp. NASA CR-54044, 1963. 

Results of Satellite Raising and Orbit 

Transfer Studies for Low Power Eiectrotkrmai 

Arc-Jet Propulsion Systems. 

Marchand, F.E.; Arthur, P.D.; HcCaughey, 0. 

AIAA Preprint 63-010, Mar. 1963. 

Applicability of Electrothermal Arc Jet 

Engines for Attitude Control and Station 

Keeping of a 550 Pound Synchronous Equatorial 

Sate1 1 i te. 

Marchand, F.E.; McCaughey, O.J. 

Plasmdyne Corp., Feb. 1963. 

Experimental Plasmajet Thruster Results. 

Masser, P.S. 

AIM J., vol. 1, no. 7, 1963, p. 1651. 

Research and Advanced Development of a 2kw 

Arcjet Thrustor. 

McCaughey, O.J.; Geideman, W.A.; Muller, K. 

Plasmadyne Corp. NASA CR-54035, 1963. 

Chemical Nonequilibriun Effects in Thermal 

Arcjet Propulsion. 

Mironer, A.; Macder, H. 

In: 

Aeronautics, vol . 9, Academic Press, Inc. , 

1963, p. 121. 

Development Progress in Astronautics and 

02:075: 1963 

02:076: 1963 

02:077:1963 

02:078:1963 

02:079: 1963 

02:080: 1963 

02:081:1964 

2:082: 1964 

02:083: 1964 

02:084:1964 

02:085:1964 

Objectives and Design of a 1-kw Arc-Jet 

Engine for Space Flight Testing. 

Page, R.J.; Hunpal, H. 

In: 

Aeronautics, vol. 9, Academic Press, Inc., 

Development Progress in Astronautics and 

1963, pp. 3-20. 

Development Work on Plasma Arcjet Engines. 

Richter, R. 

Electric Propulsion Conference, Berkeley, CA, 

Mar. 14-16, 1963, American Rocket Society, 

1963. 

Study of AC Arc Dynamics, Stabilization and 

Starting Criterion. 

Richter, R. 

General Electric Co. NASA CR-52488. 1963. 

Performance of a Constricted-Arc Discharge in 

a Supersonic Nozzle. 

Shepard, C.E.; Watson, V.R. 

AIM Paper 63-380, 1963. 

Anodic Phenanena in Nitrogen Plasma Jet. 

Tateno, H.; Saito, K. 

Jpn. J. Appl. Phys., vol. 2, 1963, p. 192. 

Theoretical and Experimental Investigation of 

Arc Plauna-Generation Technology, Part 11, 

Appiied Research on Electric Arc Phenanena. 

ASD-TRD-62-729, 1963, pp. 87-167. 

Development of a 30-kw Three Phase AC Arc Jet 

Propulsion System. 

Richter, R. 

General Electric Co. NASA CR-54112, 1964. 

Electrical Propulsion for Control of 

Stationary Satellites. 

Boucher, R.A. 

J. Spacecr. Rockets, vol. 1, no. 2, Mar.-Apr. 

1964, pp. 164-169. 

Basic Research on Gas Flows Through Electric 

Arcs - Hot Gas Contairment Limits. 

Cann, G.L.; Buhler, R.D.; Harder, R.L.; 

Moore, R.A. 

Report 64-49, Aerospace Research Laboratories, 

Mar. 1964. 

1-kU Arcjet-Engine System Performance Test. 

Ducati, A.C., et al. 

J. Spacecr. Rockets, vol. 2, no. 3, May 1964. 

Experimental Resul ts i n Hi gh-Speci f i c-lnpul se 

ThemIonic Acceleration. 

Ducati, A.C.; Gianni, G.M.; Huelberger, E. 

AIM J., vol. 2, 1964, p. 1452. 

19 
02:086:1964 

02:087:1964 

02:088: 1964 

02:089:1964 

02:090:1964 

02:091: 1964 

02:092:1964 

02 : 093 : 1964 

02:094:1964 

02:095:1964 

02:096:1964 

30 kU Arc-Jet Thrustor Research. 

James, J.P. 

Gianni ni Scientific Corp. APL-TDR-64-58, 

Har. 1964. 

Thirty Kilcuatt Plasmajet Rocket-Engine 

Development. 

John, R.R., et al. 

Avco Corp. NASA CR-54079, July 1964. 

Development of a Plasmajet Rocket Engine for 

Attitude and Orbit Control. 

McCaughey, 0. J. 

FR-112-651, Plamdyne Corp., June 1964. 

Thermal Arc-Jet Research. 

Moore, R.A. ; Cann, G.L. ; Korder, R.L. ; 

Buhler, R.D.; Gallagher. R.L. 

APL -TDR-64-55, E 1 ec t rodp t i cal S ys terns, Inc . Hay 1964. 

An Arc Tunnel Facility for the Thermal 

Analysis of An& and Cathode Regimes in an 

Electric Arc Colum. 

Pfender, E.; Wutzke, S.A.; Eckert, E.R.G. 

HTL-TR-58, Heat Transfer Laboratory Hechani cal 

Engineering Department, University of 

Minnesota. NASA CR-54080, 1974. 

Analytical Evaluation of Possible 

Noncryogenic Propellants for Electrothermal 

Thrusters. 

Schaefer, J.W.; Ferrante, J. 

NASA TN D-2253, 1964. 

Physical Phenanena and Technical Problems of 

Arcjet Engi res. 

Schoeck, P.D. 

J. Br. Interplanet. SOC., vol. 19, 1964, pp. 

33 7 -349. 

Evaluation of a Constricted-Arc Supersonic 

Jet. 

Shepard, C.E.; Watson, V.R.; Stine, H.A. 

NASA TN D-2066 I 1964. 

Analysis of Arc-Heating Phenanena in a Tube. 

Skifstad, J.G.; Murphy, S.N.B. 

IEEE Trans. Nuclear Science, vol. NS-11, Jan. 

1964, pp. 92-1033. 

Thirty kW Arc-Jet Thruster Research. 

Todd, J.P. 

Giannini Scientific Corp. APL-TDR-64-58, 

Mar. 1964. 

Application of Electrothermal Arc Jets to a 

Manned Orbiting Research Laboratory. 

Tobias, 1.; Kosson, R. 

AIM Paper 64-502, June 1964. 

02:097: 1964 

02 : 098 : 1964 

02:099:1964 

02: 100: 1965 

02:101:1965 

02:102:1965 

02:103:1965 

02:104:1965 

02:105:1965 

02: 106: 1965 

02: 107: 1966 

The Development of a Regeneratively-Cooled 

30 Kilowatt Arc Jet Engine. 

Todd, J.P.; Sheets, R.E. 

AIAA J., vol. 3, no. 1, Jan. 1965, pp. 122-126. 

Analysis of an Arcjet Exhaust. 

Van GWQ, W.H., et al. 

HcDonnel Research Division. NASA CR-54102, 

1964. 

Comparisons of Experimental and Theoretical 

Arc Colum Characteristics. 

Weber, H.E.; Pugnire, T.K. 

IEEE Trans. Nuclear Science, vol. NS-IC, Jan. 

1964, pp. 92-103. 

Double Discharge Feasibility. 

Ghai, M.L.; Pena, N.A. 

Space Dynamics Corp. NASA CR-54246, 1965. 

Arcjet Technology Research and Development. 

John, R.R., et al. 

Avco-Rad Corp. NASA CR-54687, 1965. 

High Specific Inpulse Thermal Arc Jet 

Thrustor Technology. Part 1, 

Moore, R.A.; Cann, G.L.; Gallagher, L.R. 

Electro4ptical Systems, Inc. AFAPL-TR-65-48, 

June 1965. 

Steadiness of a Plasmajet. 

Pfender. E.; Cremers. C. 

AIAA J., vol. 3, no. 7, July 1965, p. 1345. 

Thermal Analysis and Study of Arc Flow 

Interactions in the Anode Regime of an 

Electric Arc. 

Pfender, E.; Wutzke, S.A.; Shik, K.T.; 

Eddy, 1.; Eckert, E.R.G. 

Heat Transfer Laboratory Mechanical 

Engineering Department, University of 

Mi nnesota. NASA CR-54465, 1965. 

Development of a Regeneratively Cooled 30-kW 

Arcjet Engine. 

Todd, J.P.; Sheets, R.E. 

AIAA J., vol. 3, no. 1, Jan. 1965, p. 122. 

Arc-Jet Thruster for Space Propulsion. 

Wallner, Lewis E.; Czika, J., Jr. 

NASA TN D-2868, 1965. 

Recent Advances in Electrothermal and Hybrid 

El ectrot hermal -El ectranagnet i c Propul si on. 

Bennett, 5.; John, R.R. 

Proc. 4th Synp. on Advanced Propulsion 

Concepts, Gordon and Breach Science 

Publishers, Inc. (New York), 1966, pp. 125-154. 

20 
02:108:1966 

02:109:1966 

02: 110: 1966 

02: 111: 1966 

02: 112: 1966 

02: 113: 1966 

02: 114: 1967 

02:115:1967 

02:116:1967 

02:117:1968 

02:118:1968 

Study of the Energy Addition Process in a 

D.C. Arcjet. 

Bryson, R.J.; Frohlich, J.P. 

ARO, Inc. AEDC-TR-65-268, Apr. 1966. 

Design and Developnent of a Themionic 

Electric Thrustor. 

Ducati, A.C.; Jahn, R.G. ; Huehlberger, E.; 

Treat, R.P. 

Giannini Scientific Corp. NASA CR-54703, 1966. 

Variation of Ananalous Diffusion Rates fran 

an Arcjet Hall Device. 

Dunnill, W.A. 

AIM Paper 66-156, Mar. 1966. 

Laninar Arcjet Mixing and Heat Transfer: 

Theory and Experiment. 

Grey, J.; Sherman, H.P.; Williams, P.H.; 

Fradkin, D.B. 

AIM J., vol. 4, no. 6, June 1966, p. 986. 

The Laminar and Turbulent Flow of an Argon 

Arc Plasma. 

Runstadler, P.W. 

AIM Paper 66-189, Mar. 1966. 

Study of Arc-Jet Propulsion Devices. 

Van Camp, W.H., et al. 

Hcbnnell Aircraft Co. NASA CR-5491, 1966. 

A Probe for Total-Enthalpy lkasurements in 

Arcjet Exhausts. 

Esker, Donald W. 

AIM J., vol. 5, no. 8, Aug. 1967, p. 1503. 

Numerical Calculations for the 

Characteristics of a Gas Flowing Axially 

Through a Constricted Arc. 

Watson, V.R.; Pegot, E.B. 

NASA TN D-4042, 1967. 

Study of Electric-Arc Behavior with SuperImposed Flow. 

Wutzke, S.A.; Pfender, E. ; Eckert, E.R.G. 

AIM J., vol. 5, 1967, p. 707. 

Ground Testing Methods for Arc-Type 

Electrothermal Propulsion Systems, Discussing 

Test Faci 1 i ties. 

Bertolo, C.; Oggero, H. 

Atti e Rassegna Technica, vol. 22, Nov. 1968. 

Film-Cooling of a Plasm Generator Anode. 

Birkebak, R.C.; Cremers, C.J.; Shiver, W.D. 

AIAA J., vol. 6, Sept. 1968, pp. 1774-1776. 

02:119:1%8 

02: 120: 1968 

02:121:1968 

02: 122: 1968 

02:123:1969 

02: 124: 1970 

02:125:1970 

02: 126: 1970 

02: 127: 1970 

02:128:1970 

Electric Rocket Engines. 

Gilberg, L.A. 

Voennoe Izdatel 'stvo Hinisterstva Oborony SSSR 

(closcar), 1%8. 

Exploring in Aerospace Rocketry. Electric 

Propulsion. 

Kaufman, H. 

NASA TH X-52407, 1968. 

A Study of Interactions Between Electric Arcs 

and Gas Flars. 

Fhrlotte, G.L.; Cann, G.L.; Harder, R.L. 

Report 68-0049, Aerospace Research 

Laboratories, Mar. 1968. 

Thermal Analysis of Cathode and Anode Regimes 

of an WO-Arc. 

Shik, K.T. ; Pfender, E. ; Eckert, E.R.G. 

Heat Transfer Laboratory, Department of 

Mechanical Engineering, University of 

Minnesota. NASA CR-54664, 1968. 

Poisoning of La% Cathodes. 

Gallagher, H.E. 

J. Appl. Phys., vol. 40, no. 1, Jan. 1969, 

p. 44. 

Prediction of the Onset of Burnout of 

Tr;msp~ra?!~n-Coc?eO AW;. 

Cremers, C.J.; Hahan, J.R. 

AIM J., vol. 8, no. 4, Apr. 1970, p. 640. 

Correlation of High Pressure Arc Heater 

Results. 

Harder, R.L.; Cann, G.L. 

AIM J., vol. 8, no. 12, Dec. 1970, 

pp . 2220-2225. 

Influence of Surface Parameters on Anode 

Losses in Arcjets. 

Hassan, H.A.; Smith, N.S. 

AIAA J., vol. 8, no. 4, 1970, p. 657. 

Measurements with Aerodynamic Probes in 

Plasma Jets Produced by Electrothermal and 

Hall Current Accelerators. 

Krause, S. 

In: 

and Energetics Research, AGAR0 CP-38, Circa 

Publications, Inc., 1970, pp. 301-335. 

New Experimental Techniques in Propulsion 

Experimental Results of High-Current Arcs 

Driven Supersonically in Straight and 

Ci rcul ar Channel s . Sabol, A.P.; Steward, R.B.; Duckett, R.J. 

NASA TN D-6068, 1970. 

21 
02:129:1971 

02:130:1971 

02: 131: 1972 

02:132:1972 

02: 133: 1973 

02: 134: 1974 

02: 135: 1976 

02:136:1977 

02: 137: 1978 

Thrust fran Arc Jets with Self-induced 

Magnetic Fields. 

Hassan, H.A. 

AIM J., vol. 9, no. 4, Apr. 1971. 

Radiation Studies of Arc Heated Plasmas. 

Morris, J.C.; Yos, G.H. 

Report 71-9317, Aerospace Research 

Laboratories, 1971. 

Propulsive Performance of a 30 kU Arc-Jet 

Thruster Stabilized by Vortex and Hagnetic 

Forces. 

Oggero, H.V.; Bertolo, C. 

J. Br. Interplanet. SOC., vol. 25, 1972, p. 

411. 

Propulsive Performance of a 300 kU Arcjet 

Thruster Stabilized by Vortex and Mgnetic 

Forces. 

Oggero, H.V.; Bertolo, C.V. 

J. Br. Interplanet. SOC., vol. 25, 1972, pp. 

4 7 7-490. 

Preliminary Study of a Wall-Stabilized 

Constricted Arc. 

Graves, R.; Wells, W. 

NASA TH X-2700, 1973. 

Vortex Phenanena in the Arc-Jet Chamber. 

Oggero, M.V.; Sopetto, L. 

J. Br. Interplanet. SOC., vol. 27, 1974, pp. 

52 1-528. 

Physical Processes in Hollw Cathodes. 

Krishman, H. ; Jahn, R.G.; von Jaskowsky, W.F. ; 

Clark, K.E. 

AIM Paper 76-984, Nov. 1976. 

Vacuun Arc Anode Phenanena. 

Hiller, H.C. 

IEEE Transactions on Plasma Science, vol 

P5-5, no. 3, Sept. 1977. 

Theory of the Hollow Cathode Arc. 

Ferreira, C.H.; Delcroix, J.L. 

J. Appl. Phys., vol. 49, no. 4, Apr. 1978. 

02:138:1978 

02:139:1978 

02:140:1980 

02: 141: 1980 

02:142:1983 

02:143:1983 

02:144:1984 

02:145:1984 

02:146:1984 

2% 

Electric Arcs and Arc Gas Heaters. 

Pfender, E. 

Ch. 5 in: Gaseous Electronics, vol. 1, 

Academic Press, New York, 1978. 

Swirl Arc: A Model for Swirling, Turbulent, 

Radiative Arc Heater Flowfields. 

AIM J., vol. 16, no. 19, Oct. 1978, 

pp. 1068-1075. 

The Role of Swirl in Arc Heater Technology. 

Cann, G.L.; Horn, D.D. 

Instrumentation in the Aerospace Industry 

(vol. 261, Advances in Test Measurement 

(vol. 17): Part One. Proc. 26th Int. 

Instrumentation Synposiun, Instrument Society 

of America, 1980, pp. 223-234. 

Theoretical Aspects of the Vacuun Arc. 

Ecker, G. 

Ch. 7 in: Vacuum Arcs Theory and Application, 

Wiley-Interscience, New York, 1980. 

Evaluation of Single Crystal LaB6 Cathodes. 

Kato, T.; Shigetomi, A.; Watakabe, Y. 

J. Vac. Sci. Technol., Jan.-Clar. 1983, p. 100. 

A Cause of the Motion of Arcs in the Presence 

of a Magnetic Field. 

Ohtsuka, H. 

Vacuum, vol. 33, no. 3, Pergamon Press, 1983, 

p. 255-257. 

Cathode Degradation and Erosion in High 

Pressure Arc Discharges. 

Hardy, Terry; Nakanishi, S. 

NASA TH-83638, 1984, 

Axis of Metric Flar in Electric Arcjets and 

Nozzles. 

Hasser, T.S.; Peterson, R.E. 

AIM Paper 84-1385, June 1984. 

Pranising Cathode Materials for High 

Brightness Electron Beams. 

Zaima, S.; Adachi, K.; Shibata, Y. 

J. Vac. Sci. Technol., vol. 82, no. 1, Jan. - Har. 1984, p. 73. 
03:001:1947 

03:002:1952 

03:003: 1953 

03:004: 1955 

03:005:1956 

03:006:1957 

03:007:1958 

03:008: 1958 

03:009:1959 

03:OlO: 1959 

03:011:1959 

Category 3 - Related Topics 

Electrodeless Discharge and Sane Allied 

Problems. 

Babat, G.I. 

J. Inst. Electr. Eng., Jan. 1947. 

Recabination of Gaseous Ions. 

Massey, H.S.W. 

Adv. Phys., vol. 1, no. 4, Oct. 1952. 

The Dynamics and Thennodynamics of 

Compressible Fluid Flow. Volune 1 

Shapiro, A.H. 

Roland Press Co. (New York), 1953. 

Analytic Determination of the Discharge 

Coefficients of Flow Nozzles. 

Simnons, F.S. 

NACA TN 3447, 1955. 

Rocket Propulsion Elements. 

Sutton, G.P. 

2nd ed., John Wiley L Sons, Inc. (New York), 

1956, p. 77. 

Vapor Pressure Data for the lkre Cunnon 

Elements. 

Honig, R.E. 

RCA Rev., vol. 18, 1957, pp. 195-204. 

Properties of Gases at Very High 

Tenperatures. 

Amdur, I.; Mason, E.A. 

Phys. Fluids, vol. 1, no. 5, Sept. and Oct. 

1958. 

Gaseous Conductors. 

Cobi ne, J. 0. 

Dover Pub1 ications (New York) , 1958. 

Atanic Recanbination in a Hypersonic WindTunnel Nozzle. 

Bray, K.N.C. 

J Fluid kch., vol. 6, pt. 1, July 1959, pp. 

1-32. 

Preliminary Evaluation of Heliun as an 

Electric Arc Heated Propellant. 

Brogan, T.R. 

ARS J., vol. 29, no. 9, Sept. 1959. 

A Parametric Study of Certain Low-HolecularWeight Canpounds as Nuclear Rocket 

Propellants. 11. krmonia. 

Krieger, F.J. 

RM-2401, U.S. Air Force, July 1959. 

03:012:1959 

03:013:1959 

03:014: 1959 

03:015: 1960 

03:016: 1960 

03:017: 1960 

03:018:1960 

03:019:1960 

03:020:1960 

03:021:1960 

23 

A Parmetric Study of Certain Low-HolecularWeight Conpounds as Nuclear Rocket 

Propellants 111: Water. 

Krieger, F.J. 

RM-2402, U.S. Air Force, July 1959. 

Thrust of a Conical Nozzle. 

Landsbaun. E.R. 

ARS J., vol. 29, no. 3, Mar. 1959. 

Stability of Ceramics in Hydrogen Between 

4OOO and 4500 F. 

May, C.E.; Koneval, D.; Fryburg, G.C. 

NASA 3-5-59E, 1959. 

Theory and Application of Hot-Wire 

Calorimeter for Masurement of Ion Bean 

Power. 

Baldwin, L.V.; Sandborn, V.A. 

ARS Paper 1389-60, 1960. 

Plasma Carposition, Plasma Density, Enthalpy, 

and Specific Heat of Nitrogen, Nitric Oxide, 

and Air at 1, 3, 10, and 30 Atmospheres in 

the Tenperature Range 1OOO - 30 OOO K. 

Burhorn, F.; Wienecke, R. 

Z. Phys. Chm. (Leipzig), vel. 2!5, !%!I, 

pp. 269-292. 

Plasma Carposition, Plasma Density, Enthalpy, 

and Specific Heat of Oxygen at 1, 3, 10, and 

30 Atmospheres in the Temperature Range 

Between 1OOO and 30 OOO K. 

Burhorn, F.; Wienecke, R. 

2. Phys. Chem. (Leipzig), vol. 213, 1960, p. 

37. 

Analysis of the Flow and Energy Separation in 

a Turbulent Vortex. 

Deissler, R.G.; Perlmutter, M. 

Int. J. Heat Mass Transfer, vol. 1, no. 213, 

AUg. 1960, pp. 173-191. 

Chemical Non-Equilibriun Effects on Hydrogen 

Rocket Impulse at Low Pressures. 

Hall, J.G.; Eschenroeder, A.Q.; Klein, J.J. 

ARS J., vol. 30, no. 2, Feb. 1960, pp. 88-189. 

Compilation of Thermodynamic Properties, 

Transport Properties, and Theoretical Rocket 

Performance of Gaseous Hydrogen. 

King, C.R. 

NASA TN D-275, 1960. 

Boundary Layer Theory. 

Schlicting, H. 

4th ed., McGraw-Hi 11 (New York) , 1960, 

pp. 168-171. 
03:022:1960 

03:023:1961 

03:024: 1961 

03:025:1961 

03:026:1961 

03:027:1961 

03:028: 1962 

03:029: 1962 

03:030:1962 

03:031:1962 

03:032: 1962 

Miniature Enthalpy Probes for 

High-Tenperature Gas Streams. 

Vassallo, F.A. 

Paper ARL-66-0115, Aerospace Research 

Laboratories, June 1960. 

Direct Thrust and Efficiency Measurements of 

a Continuous Plasma Accelerator. 

Demetriades, S.T.; Zeimer, R.W. 

ARS J., VO~. 31, 1961, pp. 1278-1280. 

Langmuir Probes in a Flowing Low Density 

Plasma. 

French, J.B. 

Rep. no. 79, University of Toronto Institute 

of Aerophysics. AFOSR 2159, 1961. 

Theoretical Performance of Propellants 

Suitable for Electrothermal Jet Engines. 

Jack, J.R. 

NASA TN 0-682, 1961. 

Evaporation Effects on Haterials in Space. 

Jaffe, L.D. 

JPL-TR-33-161, California Institute of 

Technology, Oct. 1961. 

Stabi 1 i ty of Refractory Carpounds in Hydrogen 

Between 4500 F. and 5000 F. and Their 

Carpatibility with Tungsten. 

May, C.E.; Hoskstra, P.D 

NASA TN 0-844, 1961. 

Rheniun. 

B.W. Jonsen, ed., Elsevier Publishing Co. 

(New York), 1962. 

Development of a Thrust Measuring System for 

Elect-Thermal Rockets. 

Bauermeister, K.E.; Carter, F.V. 

In: Air Force Systems Carmand 1962 Carpendim 

of Synposiun Papers, vol. 1, Sept. 1962 

Thrust fmn Partly Ionized lbnatanic Gases. 

Beckmann, H.; Chapman, A.J. 

ARS J., Sept. 1962, pp. 1369-1373. 

The Use of Conical and Contoured Expansion 

Nozzles in Hypervelocity Facilities. 

Burke, A.F.; Bird, K.O. 

In: 

Advances in Hyperveloci ty Techniques, Plenum 

Press (New York), 1962, pp. 373-424. 

Proc. 2nd Synp. Hypervelocity Techniques; 

The Expansion of a Gas into Vacuun. 

Greenspan, H.P.; Butler, D.S. 

J. Fluid Hech., vol. 13, part 1, Hay 1962. 

03 : 033: 1962 

03:034:1962 

03:035:1962 

03:036:1962 

03:037:1962 

03:038:1962 

03 : 039 : 1962 

03:040: 1962 

03:041:1962 

03:042:1962 

03:043: 1963 

24 

Calorimetric Probe for the Measurement of 

Extremely High Temperature. 

Grey, J.; Jacobs, P.F.; Sherman, M.P. 

The Review of Scientific Instruments, vol. 33, 

no. 7, July 1962. 

Calculation of Transport Properties and Heat 

Transfer Parameters of Dissociating Hydrogen. 

Grier, N.T. 

NASA TN D-1406, 1962. 

Plasma Thermodynamics I: Properties of 

Hydrogen, Heliun, and Lithiun as Pure 

Elemental Plasmas. 

HcGee, H.A., Jr.; Heller, G. 

ARS J., Feb. 1962, pp. 203-215. 

Characteristics of Conical Supersonic 

Nozzles. 

Migdal, 0.; Landis, F. 

ARS J., VO~. 32, 1962, pp. 1898-1901. 

Reccmbination and Condensation Processes in 

High Area Ratio Nozzles. 

Olson, W.L. 

ARS J., vol. 32, 1962, p. 672. 

Thermodynamic Properties of Hydrogen from 

Roan Tenperature to 100,OOO K. 

Rosenbaum, B.M.; Levitt, L. 

NASA TN D-1107, 1962. 

High Tenperature Thermodynamic Properties of 

Selected Gases. 

Rudin, H.; Ragent. B. 

ARL-62-358, Aeronautical Research 

Laboratories, May 1962. 

Estimated Viscosities and Thermal 

Conductivities of Gases at High Tenperatures. 

Svehla, R.A. 

NASA TR-132, 1962. 

Measured Steady-State Performance of water 

Vapor Jets for Use in Space Vehicle Attitude 

Control Systems. 

Tinling, B.E. 

NASA TN D-1302, 1962. 

Experimental Determination of the Hydrogen 

Reccmbi nation Constant. 

Widawsky, A. ; Oswal t, L.R. ; Harp, J. L., Jr. 

ARS J., D~C. 1962, pp. 1927-1929. 

Electric Propulsion Development. 

In: Progress in Astronautics and 

Astronautics, vol. 9, Martin Sumnerfield, ed., 

Academic Press (New York), 1963. 
t 

03:044: 1963 Catalysis of Hydrogen Atan Recabination. 

Girouard, H. ; Graber, F.H.; Myers, B.F. 

AE63-0078, Space Science Laboratory, NASA 

Contract NAS8-2534, Feb. 1963. 

03:045: 1963 Nozzle Contours for Minim Particle-Lag 

Loss. 

Chrble, E. 

AIM J., vol. 1, 1963, p. 2793. 

03:046:1963 Thenmdynamic Properties of 6O00 K for 210 

Substances Involving the First 18 Elements. 

McBride, B.D.; Heimel, S.; Ehlers, J.G.; 

Gordon, S. 

NASA SP-3001, 1963. 

03:047: 1963 Sublimation of Tungsten in Hydrogen. 

Short, G.R.; Howard, J. 

AIM Preprint 63-024, Har. 1963. 

03:048: 1963 Convergent-Divergent Nozzle Discharge 

Characteristics in the Transition Regime 

Between Free klecule and Continuun Flow. 

Smetana, F.O. 

ASHE Paper 63-W-94, 1963. 

03:049: 1963 Conpilation of Theoretical Rocket Performance 

for the Chemically Frozen Expansion of 

Hydrogen. 

Spisz, E.W. 

NASA TN 0-2080, 1963. 

03:050: 1963 Rocket Propulsion Elements. 

Sutton, G.P. 

3rd ed., Wiley, New York, 1963. 

03:051: 1964 Electrical Propulsion for Control of 

Stationary Sate1 1 i tes. 

Boucher, R.A. 

J. Spacecr. Rockets, vol. 1, no. 2, Chr.-Apr. 

1964, pp. 164-169. 

03:052: 1964 An Evaluation of Vapor-Deposited Tungsten 

Tubing. 

Mills, R.G.; Lindgren, J.R.; Weinberg, A.F. 

John Jay Hopkins Laboratory for Pure and 

Applied Science. NASA CR-54277, 1964. 

03:053: 1964 Nozzle Characteristics in the Transition 

Regime Between Continuun and Free klecular 

Flw. 

Milligan, M.W. 

AIM J., 1964, pp. 1088-1092. 

03:054: 1964 Analytical Evaluation of Possible 

Noncryogenic Propellants for Electrothermal 

Thrusters. 

Schaefer, J.W.; Ferrante, J. 

NASA TN D-2253, 1964. 

03:055:1965 Effect of Pressure on Rate of Burning of 

Liquid Hydrazine. 

Antoine, A.C. 

NASA TN 0-2694. 1965. 

03:056:1965 Canparison of Measured and Predicted Flan 

Through Conical Supersonic Nozzles, with 

ERphasis on the Transonic Region. 

Back, L.H.; hssier, P.F.; Gier, H.L. 

AIM J., vol. 3, no. 9, Sept. 1965, 

p~. 1606-1614. 

03:057:1965 Diagnostic Studies in a Hall Accelerator at 

Lw Exhaust Pressure. 

Brockman, P.; Hess, R.; Bwen, F.; Jarrett, 0. 

AIAA Preprint 65-297, July 1965. 

03:058:1965 Expansion of a Jet into Near Vacuun. 

Cassanova, R.A.; Stephenson, W.B. 

AEDC-TR-65-151, ARO, Inc., Aug. 1965. 

03:059:1965 Space Envinmnent Facility for Electric 

Propulsion Systems Research. 

Finke, R.C.; Holmes, A.O.; Keller, T.A. 

NASA TN D-2774, 1%5. 

03:060: 1965 High Temperature Electrical Properties of 

Insulators and Their Carpatibility with 

Refractory Cktals. 

Ciaveii, R.F.; Hoitz, F.C. 

111 Research Institute (NASA CR-54125). Chr. 

1965. 

03:061: 1965 Thennodynanic Properties of Hydrazine. 

Haws, J.L.; Harden, D.G. 

AIM J. of Spacecraft, vol. 2, no. 6, 

NOV.-DeC. 1965. 

03:062:1965 Gas Dynanic Problems in Low Pressure 

Mi crothrust Engi nes. 

Jonath, A.D. 

Astronautica Acta, vol. 11, no. 5, Sept.-Oct. 

1965, p. 348. 

03:063:1965 Gasdynamic Problems in Low Pressure 

Microthrust Engines. 

Jonath, A.D. 

AIAA Paper 65-616, 1965. 

03:064: 1966 Control Logic for Atti tude Control of a Space 

Vehicle. Volw 111. 

Dazzo, J.J.; Hall, C.E. 

Proc. 13th Ann. AF Science and Engineering 

Symp., 1966. 

03:065:1966 Propulsive Performance of a Cold Gas Attitude 

Control Reaction Jet System. 

Greer, H. 

J. Spacecr. Rockets, vol. 3, 1966, pp. 429-431. 

25 
03:066:1966 

03:067: 1966 

03:068:1966 

03:069:1966 

03:070:1966 

03:071:1967 

03:072:1967 

03:073: 1967 

03:074: 1967 

03:075: 1967 

03:076: 1967 

03:077:1967 

Measured Performance of Water Vapor Jets for 

Space Vehicle Attitude Control Systems. 

Kanning, G. 

NASA TN D-3561, 1966. 

Advanced Propulsion/Reaction Control System 

Study for a knned Orbiting Research Laboratory. 

Pisciotta, A., Jr. et al. 

AIAA Paper 66-579, June 1966. 

Boundary Layers and Their Interaction in 

Rotating Flows. 

Rott, N.; Lewellen, W.S. 

In: Development Progress in Aeronautical 

Sciences, vol. 7, pp. 111-144, Pergmn Press, 

1966. 

Sane Innovations in Thrust Balance Design. 

Sinnette, J.T., Jr.; Stoner, W.A. 

AIM Paper 66-228, Mar. 1966. 

A Review of Microrocket Technology. 

Sutherland, G. S.; Macs, M. E. 

J. Spacecr. Rockets, vol. 3, Aug. 1966, pp. 

1153-1 165. 

Development of the Subliming Solid Control 

Rocket, Phase 11. 

Rocket Research Corp. NASA CR-712, 1967. 

Radioisojet Program Sunnary Report. 

NASA TM X-63018, 1967. 

Performance of Two Sub1 iming-Sol id-Propellant 

Thrustor Systems for Atti tude Control of 

Spacecraft . Berkopec, F.D. 

NASA TN 0-3841, 1967. 

Investigation of Dynamic Rocket Thrust 

kasurement Techniques. 

Crosswy, F.L.; Kalb, H.T. 

AEDC-TR-67-202, Arnold Engineering Development 

Center, Nov. 1967. 

Direct Microthrust kasurement on "Swinging 

Gate" Test Stand. 

Cutler, W. 

Space/Aeronautics, vol. 47, Mar. 1967, pp. 

115, 116,119. 

Orbit Trim Propulsion Requirements for Sun 

Synchronous Sate1 1 i tes. 

Endres, D.L. 

NASA TM X-55825, 1967. 

MORL Design Studies - The Significant 

Results. 

Gardner , W. N . Astronaut. Aeronaut., vol. 5, no. 3, Mar. 

1967, pp. 34-46. 

03:078:1967 

03:079:1967 

03:080:1967 

03:081: 1968 

03:W2:1968 

03:083: 1968 

03:084:1968 

03:085:1968 

03:086:1968 

03:087:1968 

03:088: 1969 

26 

Dynamic Performance of Low-Thrust, Cold-Gas 

Reaction Jets in a Vacuun. 

Greer, H.; Griep, D.J. 

J. Spacecr. Rockets, vol. 4, no. 8, Aug. 67, 

pp. 983-990. 

Handbook of Materials and Techniques for 

Vacuun Devices. 

Kohl, W.H. 

Reinhold Publishing Corp. (New York), 1967. 

Miniature Probes for the Instantaneous 

Measurement of Enthalpy in Arc Jets. 

Vassallo, F.A. 

ARL-67- 0181, Aerospace Research Laboratories, 

Sept. 1967. 

A Preliminary Study of Vapor Deposition of 

Rheniun and Rheniun Tungsten. 

Donaldson, J.F.; Hoertel, F.W.; Cochran. A.A. 

J. Less-Comnon Met., vol. 14, 1968. 

Optimal Space Flight with Multiple Propulsion 

Hazelrigg, G.A., Jr. 

J. Spacecr. Rockets, vol. 5, Oct. 1968, pp. 

Systems. 

1233-1235. 

Physics of Electric Propulsion. 

Chapter 6, McGraw-Hill, New York, 1968. 

Performance Losses in Low-Reynol ds-Nunber 

Nozzles . Murch, C.K. 

J. Spacecr. Rockets, vol. 5, no. 9, Sept. 

1968, pp. 1090-1094. 

Doppler Measurements of the Exhaust 

Velocities in an MPD Thruster. 

Sovie, R.J.; Connolly, D.J. 

Bulletin of American Physical Sciences, 

vol. 13, no. 11, Nov. 1968, p. 1513. 

Conception and Experimentation of an 

Electrothermal System of Orbital Propulsion. 

Thieck, J. 

Paper P-175, International Astronautical 

Federation, Oct. 1968. 

Tables of Sane Supersonic Gas Flow Functigns. 

Walton, R. 

RAE-TR-68245, Royal Aircraft Establishment, 

Oct. 1968. 

Final Report on a Study of Low-Density Nozzle 

Flows, with Application to Microthrust 

Rockets. 

Cornel1 Aeronautical Lab., Inc. 

NASA CR-107299, 1969. 
03:089:1969 

03:090:1969 

03:091:1969 

03:092: 1969 

03:093:1969 

03:094:1969 

03:095:1969 

03:096: 1969 

03:097: 1969 

03:098: 1969 

The Effect of Background Pressure and 

Magnetic Field Shape on MPD Thruster 

Performance. 

Connolly, D.J.; Sovie, R.J. 

AIAA Paper 69-243, Mar. 1969. 

Theoretical Analysis of Electrothermal 

Thrusters with Supersonic Heat Addition. 

Leon, H.I.; Mickelsen, W.R. 

AIM Paper 69-286, Mar. 1969. 

Analog Systems of Tenperature Fields in 

Plane. 

flickelsen, W.R. 

Colorado State University (NASA CR-107484 

REPT-81, May 1969. 

Electric Propulsion Mission Analysis. 

flullin, J.P., et al. 

NASA SP-210, 1969. 

Sane Nunerical Results on Viscous Low-Density 

Nozzle Flows in the Slender-Channel 

Approximation. 

Rae, W.J. 

AIAA Paper 69-654, June 1969. 

Experimental Performance of a WaterElectrolysis Rocket. 

Rollbuhler, R.J. 

NASA Tfl X-1737, 1969. 

Applications of Some Refractory Metals in 

Space Technology. 

Sherwood, P.J. 

Presented at the 3rd British Interplanetary 

Society Synposiun on Materials in Space 

Technology, Bristol, England, Apr. 9-11, 1969. 

Onboard Ricrothrustors State of Developnent 

and Comparative Analysis of Fields of 

Uti 1 i zat ion. 

Souquet, J. 

Congres International Aeronutique, 9th, Paris, 

June 2-4, 1969, Association Francaise des 

Ingenieurs et Technicienc de 1 'Aeronautique et 

de I'Espace, June 1969 (in French). 

A Study of the Axial Velocities in an Amnia 

MPD Thruster. 

Sovie, R.J.; Connolly, D.J. 

AIM J., vol. 7, no. 4, Apr. 1969, pp. 723-725. 

Conical Nozzle Flow with Velocity Slip and 

Temperature Junp. 

Williams, J.C. 

Errata, AIM J., vol. 7, no. 2, 1969, p. 384) 

AIAA J. VOl. 5, 1967, pp. 2128-2134 (SW 

03:099:1970 

03: 100: 1970 

03: 101 : 1970 

03: 102: 1970 

03:103:1970 

03: 104: 1970 

03:105:1970 

03:106:1970 

03: 107: 1970 

03:108:1970 

27 

Trade-off Study and Conceptual Designs of 

Regenerative Advanced Integrated Life Support 

systems - 

NASA CR-1458, 1970. 

Kinetics and Thermodynamics in HighTenperature Gases. 

NASA SP-239, 1970. 

Propulsion. 

Space/Aeronautics, vol. 54, July 1970, 

pp. 21-25. 

Swirling Flow Through a Nozzle. 

Batson, J.L.; Sforzini, R.H. 

J. Spacecr. Rockets, vol. 7, no. 2, Feb. 1970, 

pp. 159-163. 

USAF Propellant Handbodts. 

Hydrazine Fuels, vol. 1, Bell Aerospace Co. 

AFRPL-TR-69-149, Mar. 1970. 

Prediction of the Onset of Burnout of 

Transpiration-Cooled Anodes. 

Cremers, C.J.; Mahan, J.R. 

AIAA J., vol. 8, no. 4, Apr. 1970, p. 640. 

Nuclear Electric Rockets. 

Loeb, H. 

Rockets, W. Hanle and M. Pollermann, eds., 

Giessen, Universitaet, Giessen (West Germany), 

In: #uc!ear Engineering far =-A^'': JaLrl I ltes and 

1970, pp. 228-275. 

Viscous Effects on the Flou Coefficient for a 

supersonic Nozzle. 

Massier, P.F.; Back, L.H.; Noel, M.B.; 

Raheli, F. 

AIAA J., vol. 8, no. 3, Mar. 1970, pp. 605-607 

Electrothermal Thrustor with a Liquid 

Propellant. 

Morin, R.; Thieck. J.; Valentian, D. 

International Technical and Scient if ic 

Conference on Space, 10th. Rune, Italy, Mar. 

9-1 1, 1970, Rassegna Internazionale e 

El ettroni ca Nucl eare e Teleradioci nematografica, 1970. 

Electron-Beam Studies of Low Reynolds Nunber 

Flows Inside a DeLaval Nozzle. 

Rothe, D.E. 

AIAA Paper 70-810, 1970. 
03:109:1970 

03:110:1971 

03: 111: 1971 

03:112:1971 

03: 113: 1971 

03: 114: 1971 

03: 115: 1971 

03: 116: 1971 

03: 117: 1971 

Electronic Propulsion Systems for Long-Term 

Space Station Operations. 

Stuhlinger, E. 

Proc. Int. Academy of Astronautics, Orbital 

Internationa: Lab, and Space Sciences 

Conference, Cloudcroft, NM, Sept. 2843. 2, 

1969, AFMDC Publishing Management Branch, 

1970, pp. 464-482. 

Flow Coefficients for Supersonic Nozzles with 

Conparatively Small Radius of Curvature 

Throats. 

Back, H.L.; Cuffel, R.F. 

J. Spacecr. Rockets, vol. 8, no. 2, Feb. 1971, 

pp. 196-198. 

Skylab Attitude and Pointing Control System. 

Chubb, W.B.; Seltzer, S.M. 

NASA TN 0-6068, 1971. 

A Chparative Study of Chemical and 

Nonchemical Propulsion Systems for Attitude 

Control and Orbit Correction of Geostationary 

Satellites in the 500 to 1OOO kg Class. 

Part 8: Application of the Propulsion 

Systems to a Particular Satellite 

Configuration. 

Fraga, E.; Crespo, A. 

ESRO-CR-38, Insti tuto Nacional de Technica 

Aerospacial, July 1971. 

Satellite Auxiliary Propulsion Selection 

Techniques - Addendun: Survey of Auxiliary 

Electric Propulsion Systems. 

Holccmb, L.B. 

NASMJPL TR 32-1505, 1971. 

Supersonic Nozzle Discharge Coefficients at 

Low Reynolds NWrs. 

Kuluva, N.M.; Hosack, G.A. 

AIM J., vol. 9, no. 9. Sept. 1971. 

An Experimental Investigation of Superheated 

Sub1 iming Sol id Thruster Performance. 

Owens, W.L., Jr. 

J. Spacecr. Rockets, vol. 8, no. 7, July 1971, 

pp. 806-809. 

Thermodynamic Properties and Theoretical 

Rocket Performance of Hydrogen to 100 OOO K 

and 1.01325~108 N/d. 

NASA SP-3069, 1971. 

Final Report on a Study of Low-Density Nozzle 

Flows, with Application to Microthrust 

Rockets. 

Rae, W.J. 

AIM J., vol. 9, no. 5, May 1971, pp. 811-820. 

03: 118: 1971 

03:119:1971 

03:120:1971 

03:121:1972 

03:122:1972 

03: 123: 1972 

03:124:1972 

03:125:1972 

03: 126: 1972 

03: 127: 1972 

28 

Electron-Bean Studies of Viscous Flow in 

Supersonic Nozzles. 

Rothe, D.E. 

AIM J., vol. 9, no. 5, May 1971, pp. 804-811. 

Design and Developnent of a Micropovnd 

Extended Range Thrust Stand (MERTS) . Stark, K.W. ; Dennis, T. ; McHugh, D. ; 

Williams, T. 

NASA TN 0-7029, 1971. 

A Carparative Study of Chemical and 

Nonchemical Propulsion Systems for Attitude 

Control and Orbit Correction of 

Geostationary Satellites in the 500 to 

1OOO kg Class. Part A: Statement of the 

Characteristics of the Propulsion Systems. 

Tarifa, C.S.; Urrutia, J.L.; Fraga, E.; 

Hunoz, A.; Crespo, A. 

ESRO-CR-25-PT4, Insti tuto Nacional de 

Technica Aerospacial, July 1970. 

nodular Space Station Phase B Extension - Preliminary System Design. 

Volume VI, Trades and Analysis, North American 

Rockwell. NASA CR-115411, 1972. 

Ibnopropellant Hydrazine Propulsion Systems 

Sessions. 

1972 JA"AF Propulsion Meeting. CPIA Publ. 

no. 228, vol. IV, Chemical Propulsion 

Information Agency, Dec. 1972. 

The 1972 JA"AF Propulsion Meeting, 

Mobnopropellant Hydrazine Propulsion Systems 

Sessions. 

CPIA Publ. 228, vol. IV, Chemical Propulsion 

Information Agency, Dec. 1972. 

Influence of Contraction Section Shape and 

Inlet Flow Direction on Supersonic Nozzle 

Flow and Perfotmance. 

Back, L.H.; Cuffel, R.F. ; Massier, P.F. 

J. Spacecr., vol. 9, no. 6, June 1972. 

Thruster Characterization Using a Thrust 

Balance. 

Bailey, A.G. 

Rev. Sci. Instrum., vol. 43, no. 12, Dec. 1972. 

DART Technology Developnent. 

Cooper, K.C.; Turner, W.C. 

LA-5017-MS, Los Alms Scientific Laboratory 

of the University of California, Dec. 1972. 

System Study of Electric Propulsion for 

Military Space Vehicles. 

Hawk, C.W.; Bary, R.S.; Rosen, S.G.; 

Quirk, J.A. 

AIM Paper 72-493, 1972. 
03:128:1972 

03:129:1972 

03: 130: 1972 

03:131:1972 

03:132:1972 

03:133:1972 

03: 134: 1972 

03:135:1972 

03:136:1972 

03: 137: 1972 

Survey of Sate1 1 i te Auxi 1 iary Propulsion 

Systems. 

Holconb, L.G. 

J. Spacecr. Rockets, vol. 9, hr. 1972, pp. 

133-1 47. 

Optimisation of Geostationary Satellite 

Enplacement by Lou Thrust Propulsion. 

Holdaway, R.; Jansson, R.E.W. 

Southarrpton Univ. (England), Sept. 1972. 

The Design and Development of a Miniature 

Bi-Stable Latching Solenoid Valve for Lou 

Thrust Resistojets. 

Lynch, R.A. 

Marquardt Corp. NASA CR-112161, 1972. 

Evaluation of Zirconia, Thoria, and Zirconiun 

Diboride for Advanced Resistojet Use. 

Page, R.J.; Short, R.A.; Halbach, C.R. 

NASA CR-112075, 1972. 

Experimental Performance of Supersonic 

Nozzles Using Lithiun Vapor as a Propellant. 

Roehling, D.J.; Stratton, T.F.; Fradkin, D.B. 

AIM Paper 72-453, Apr. 1972. 

Progressive Attitude and Orbit Correction 

with the Aid of Hydrazine - Propulsion 

Systems and Their ERploynent in Eu-. 

Schmitz, H.; Woidneck, H. 

DGLR Paper 72-078, Deutsche Gesellschaft fuer 

Luft- und Ramfahrt, Oct. 1972. 

The Removal of Impurities fran Hydrazine for 

Control of Contamination Caused by Rocket 

Engine Exhaust. 

Schuler, W.B.; Pharo, T.J.; Hall, C.A. 

AIAA Paper 72-1046, 1972. 

Thrust Measurements of a Hollow-Cathode 

Discharge. 

Snyder, A.; Banks, B.A. 

NASA TN D-6705, 1972. 

Hydrazine Propulsion System for Applications 

Satellite (ATS) 3, 4, and 5. 

Suddeth, D.H.; Sievers, R.W. 

In: 1972 JA"AF Propulsion Ileeting. CPIA 

Publ. 228, vol. IV, Chemical Propulsion 

Information Agency, Dec. 1972, pp. 85-96. 

Vacuun Hicrobalance Techniques. Volune 2. 

Warner, A.W.; Stockbridge, C.D. 

R.F. Walker, ed., Plenum Press (New Vork), 

1972. 

03: 138: 1972 

03:139:1973 

03:140:1973 

03:141:1973 

03: 142: 1973 

03: 143: 1973 

03:144:1973 

03:145:1974 

03:146:1974 

03: 147: 1974 

Atmospheric Drag Cross-section of Spacecraft 

Solar Arrays. 

Williams, R.R. 

J. Spacecr. Rockets, vol. 9, no. 8, Aug. 1972, 

p~. 565-566. 

Models of the Earth's Atmosphere (120 to 

loo0 km). 

NASA SP-8021, 1973. 

Ascent Phase and Orbital Correction 

Propulsion -le. 

Balzer, D.L.; Belsley, A.C. 

AIM Paper 73-1267, 1973. 

Wideband Thrust and Transient Inpulse 

Heasurement of Electrothermal Gasdynamic and 

Pulsed Plasma Thrusters. 

Barber, B.C. 

AIAA Paper 73-1065, Oct. 1973. 

Thermal Insulation for Electrothermal 

Thrusters. 

Dixon, J.C.; Nusgrove, P.J. 

In: 

Space Vehicles, Institution of Electrical 

Engineers (England), 1973, pp. 166-170. 

Proc. Conf. on Electric Propulsion of 

Performance Characterization Tests of Three 

8.444 (0. l-lbf) Hydraiine Catalytic 

Thrusters. 

Mynihan, P.I.; Bjorklund, R.A. 

JPL-TR-32-1584, Sept. 1973. 

Striated Nozzle Flow with Small Radius of 

Curvature Ratio Throats. 

Norton, D.J.; White, R.E. 

J. Spacecr. Rockets, vol. 10, no. 11, 

NOV. 1973, pp. 747-750. 

Thrust Measuring System for Electrothermal 

Trusters. 

Barber, B.C. 

J. Spacecr. Rockets, vol. 11, no. 8, Aug. 

1974, pp. 549-553. 

An Integrated Nuclear Elect-Thermal Engine 

Concept for Geostationary Mi ssions. 

Bond, A. 

In: Third European Electric Propulsion 

Conference, Deutsche Gesellschaft fuer Luftund Ramfahrt (Cologne), 1974, pp. 250-253. 

Status of the Development of Electrical 

Propulsion Systems for Space Travel. 

Lwb, H. 

DGLR Paper 74-71, Deutsche Gesellschaft fuer 

Luft- und Ramfahrt (Cologne), Sept. 1974. 

29 
03:148:1974 

03:149:1975 

03:150:1975 

03:151:1975 

03:152:1975 

03: 153: 1975 

03: 154: 1975 

03: 155: 1975 

03: 156: 1975 

03: 157: 1976 

03: 158: 1976 

She1 1-405 Catalyst Improvement. 

Meetin, R.J.; Newton, N.C. 

AFRPL-TR-74-36, July 1974. 

The Secondary Propulsion Subsystem for the 

Broadcast Satel 1 i te Experimental. 

Abbott, E., et al. 

AIM Paper 75-1191, 1975. 

Direct Thrust Heasurement of a 30411 Ion 

Thruster. 

Banks, 6.; Rawlin, V.; Weigand, A.; Walker, J. 

NASA TH X-71646, 1975. 

Hydrazine Engine Plune Contamination 

hppi ng . Chirivella, J.E. 

AFRPL-TR-75-16, OCt. 1975. 

Nonopropel lant Hydrazine Propulsion Subsystem 

for the Fleet Satellite Cannunications 

(Fltsatcan) Spacecraft. 

Fritz, 0.; Sackheim, R.; Bassichis, J. 

AIM Paper 75-1228, Oct. 1975. 

Electric Rocket Engines - Russian Book. 

Grishin, S.O.; Leskov, L.V.; Koslov, N.P. 

Izdatel 'stvo Hashinostroenie (Moscow) , 1975 

(in Russian). 

New Directions in Autmted Spacecraft Cost 

Estimation. 

Pekar, P.P. 

J. Spacecr., vol. 12, no. 8, Aug. 1975, pp. 

458-464. 

The ESA Activities in the Field of Hydrazine 

Monopropel lant Technology for Satel 1 i te 

Auxiliary Propulsion. 

Pfeffer, H.A. 

AIM Paper 75-1227, Sept. 1975. 

Hydrazine/Haterial Campatibility. 

Williams, L.O.; Anselmi, R.T. 

AIAA Paper 75-1245, 1975. 

Propellant/Haterial Campatibility Program and 

Results. 

JPL Tech. rtemo 33-770, Aug. 1976. 

Determination of Long-Term Carpat i bi 1 i ty of 

Hydrazine with Selected Haterials of 

Construction. 

Brown, C.T. 

AFRPL-TR-76-33, June 1976. 

03: 159: 1976 

03: 160: 1976 

03: 161 : 1976 

03: 162: 1976 

03:163:1976 

03:164:1976 

03: 165: 1976 

03:166:1977 

03: 167: 1977 

03: 168: 1977 

ESA Activities in the Field of Hydrazine 

Nonopropel lant Technology for Satel 1 i te 

Auxiliary Propulsion. 

Pfeffer, H.A. 

ESA Sci Tech. Rev., vol. 2, no. 1, 1976, 

pp. 43-54. 

5 Pound Thrust Non-Catalytic Hydrazine 

Engine. 

Pugnire, T.K.; O'Connor. T.J. 

AIAA Paper 76-660, July, 1976. 

0.2 lbf Monopropellant Thruster Tests with 

MIL Grade and Viking Grade Hydrazine. 

Richards, R.E.; Grabbi, R. 

AIAA Paper 76-657, July 1976. 

Flight Performance of the Hydrazine Reaction 

Control Subsystem for the Cannunications 

Technology Satel 1 i te. 

Sansevero, V.J., Jr.; Garfinkel, H. 

AIM Paper 76-630, July 1976. 

ATS-6 Propulsion: 

Schreib, R.R. 

AIAA Paper 76-629, 1976. 

Two Years in Orbit. 

Performance and Heat Transfer Characteristics 

of the Laser-Heated Rocket: A Future Space 

Transportation System. 

Shoji, J.H.; Larson, V.R. 

AIM Paper 76-1044, Nov. 1976. 

Thermal Hydrazine Decanposition - Studies 

Regarding Alternative Solutions for Atti tude 

Control Systems. 

Twardy, H. 

OGLR Paper 76-190, Deutsche Forschungs- und 

Versuchsanstalt fuer Luft- und Raumfahrt, 

Sept. 1976. 

Nonopropellant Thruster Exhaust Plune 

Contami nation Measurements. 

Baerwald, R.K.; Passmneck, R.S. 

AFRPL-TR-77-44, Svt. 1977. 

A Fast Response Thrust Transducer for 

Gasdynami c Thrusters. 

Barber, B.C. 

RAE-TR-77025, Royal Aircraft Establishment, 

Feb. 1977. 

The Fundamentals of Chemical Vapour 

oeposi t ion. 

Bryant, W.A. 

J. Mater. Sci., vol. 12, 1977, pp. 1285-1306. 

30 
03: 169: 1977 

03: 170: 1977 

03:171:1977 

03: 172: 1977 

03: 173: 1977 

03:174:1977 

03: 175: 1978 

03: 176: 1978 

03: 177: 1978 

The Effect of Hydrazine karposition 

Products on the kchanical Properties of 

High-Tenperature A1 loys. 

Chandler, W.T. 

AFflL-TR-77-95, flay 1977. 

Design Criteria knual for Long-Life 

Monopropellant Engines. 

Emnons, D.L. 

AFRPL-TR-77-6, 1977. 

Performance of Low Thrust Attitude Control 

Engines. Part 4: Correlation Equation for 

Experimental Boundary Layer Losses. 

Hayn, D.; Schmucker, R.H. 

TUn-LRT-TB-77/14-PT-4, Technische University, 

Oct. 1977. 

The NASA Standard 5-Newton Hydrazine 

Thruster. 

Jones, L.W., et al. 

AIAA Paper 77-962, 1977. 

Thermal Hydrazine Decarposition: 

Investigation on a Pranising Technique for 

Future Satel 1 i te Propulsion. 

Twardy, H. 

In: Altitude and Orbit Control Systems. 

ESA-SP-128, European Space Agency, Paris, 

France, 1977, pp. 479-487. 

Hydrazine Thrusters for Space Applications. 

Valentini, R. 

In: Attitude and Orbit Control Systems, 

ESA-SP-128, European Space Agency, Paris, 

France, 1977, pp. 435-444. 

WS Propulsion Mule Design. 

Barker, F.C.; Schreib, R.R. 

AIM Paper 78-1095, 1978. 

Hot Burst Strength of Vapour Deposited 

Rheniun - for Tube Applications. 

Wry, A.; Hayman, C.; Kent, P.J.C. 

J. Br. Interplanet. SOC., vol. 31, Feb. 1978, 

pp. 57-59. 

Analysis and Design Study of the Hultimission 

Modular Spacecraft Hydrazine Propulsion 

Wule. 

Etheridge, F.G. 

AIM Paper 78-1094, July 1978. 

03: 178: 1978 Data Sources for Haterials Scientists and 

Engineers. 

Westbrook, J.H.; Desai, J.D. 

Annu. Rev. Hater. Sci., vol. 8, 1978, pp. 

359-422. 

03:179:1979 

03:180:1979 

03: 181 : 1979 

03:182:1979 

03:183:1979 

03: 184: 1979 

03:185:1979 

03: 186: 1980 

03: 187: 1980 

Bi propel 1 ant Engine P1 me Contani nation 

Progran. 

Alt, R.E. 

AEDC-TR-78-28, VOl. 1, DeC. 1979. 

The Nonopropellant Hydrazine PrOpUlSiOn 

Subsystem for the Pioneer Venus Spacecraft. 

Barker, F.C. 

AIAA Paper 79-1329, 1979. 

Characteristics of Primary Electric 

Propulsion Systems. 

Byers, D. 

NASA Tfl-79255, 1979. 

Stabilization Systems for Future 

cannunication Satel 1 i tes. 

Lac-, fl.; Runavot, fl. 

In: Space, Space Telecmnications and 

Satel 1 i te Radio Broadcasting: Objectives for 

the Next Decade, Centre National D'Etudes 

Spatiales (Toulouse, France), 1979, pp. 607- 

617. 

Optical Properties of Bipropellant Exhaust 

Constituents Condensed at 77 K. 

Roux, J.A.; Wood, R.E.; Alt. R.E.; 

Frazine, 0. F. 

J. Spacecr., vol. Ib, no. 6, Nov.-Dec. i9i9, .. 

pp. 373-381. 

Design and Flight Performance of the 

Hydrazine Auxiliary Propulsion System for the 

International Ultraviolet Explorer Satellite. 

Sansevero, V.J., Jr.; Garfinkel, H. ; 

Wojnarowski, J. 

AIM Paper 79-1300, June 1979. 

Characterization Testing of a 0.20 lbf 

Hydrazine Thruster. 

Vancamp, V.V. 

AIM Paper 79-1306, June 1979. 

Large Space Systems/Low-Thrust Propulsion 

Techno1 ogy . NASA CP-2144, 1980. 

Evaluation of an Electrothermal Hydrazine Gas 

Generator for Attitude Control of Spacecraft. 

Breves, E.O. 

Erno Raunf ahrt techni k G .m. b . H . VB-042 10 18-B 

ESA-CR(P)-1357, Apr. 1980. 

03: 188: 1980 Propulsion Subsystem for the flulti-Hission 

Wular Spacecraft (WS). 

Finston, R.; Spicer, L.fl. 

AIM Paper 80-1291, July 1980. 

31 
03: 189: 1980 

03:190:1981 

03: 191: 1981 

03:192:1981 

03: 193: 1981 

03: 194: 1981 

03:195:1982 

03: 196: 1982 

03:197:1982 

03: 198: 1983 

Hydrogen Permeability Through Rheniun and an 

We Alloy With and Without Chemically 

Vapor-Deposi ted Tungsten Coatings. 

Svedberg, R . C . Thin Solid Films, vol. 72, 1980, pp. 385-392. 

Monomethyl hydrazine Versus Hydrazine Fuels: 

Best Results Using a lOelbf Bipropellant 

Rocket Eng i ne. 

AIM Paper 81-1573, July 1981. 

A Review of Future Orbit Transfer Technology 

for Space Industrialization. 

Fearn, D.G. 

RAE-TR-81080 RAE-SPACE-599, Royal Aircraft 

Establ i shnt , June 1981. 

Propulsion Subsystem for the Hultimission 

Hcdular Spacecraft (MS) . Finston, R.; Spicer, L.H. 

J. Spacecr., vol. 18, no. 4, Aug. 1981, 

pp. 344-349. 

Tests of Spacecraft Electromket Engine 

Systems - Russian Book. 

Iakovlev, E.A. 

Izdatel 'stvo Hashinostroenie (Moscow), 1981. 

Study of Electrical and Chemical Propulsion 

Systems for Auxiliary Propulsion of Large 

Space Systems. 

Smith, W.W.; Clark, J.P. 

Boeing Aerospace Co. NASA CR-165502-VOL-1, 

1981. 

Evolutionary Space Science Concept Study. 

HcDonnell-Douglas Astronautics Co. 

NASA CR-170829, 1982. 

Space Operations center (SKI System 

Analysis Study Extension. 

Boeing Aerospace Research. NASA CR-167555, 

1982. 

Camunication Satellite Propulsion Evolution 

and Options. 

Schreib, R. 

AIM Paper 82-1193, June 1982. 

Contamination kasurements During Operation 

of Hydrazine Thrusters on the P78-2 (SCATHA) 

Sate1 1 i te. 

Carre, D.J.; Hall, D.F. 

J. Spacecr., vol. 20, no. 5, Sept.-Oct. 1983. 

03: 199: 1983 

03:200:1983 

03:201:1983 

03:202:1983 

03: 203 : 1983 

03 : 204 : 1983 

03:205:1984 

03:206:1984 

03:207: 1984 

03:208:1984 

Space Station Propulsion System Trade Study. 

Garrison, P.W.; Klemetson, R.W. 

AIM Paper 83-1220, June 1983. 

Design Surmary of the Intelsat V Spacecraft. 

Hoeber, C.F.; Barberis, N.J. 

J. Spacecr., vol. 20, no. 4, July- Aug. 1983. 

Space Station orbit Maintenance. 

Kaplan, D.I.; Jones, R.H. 

AIAA Paper 83-0347, Jan. 1983. 

Auxi 1 iary Propulsion Requirements for Large 

Spacecraft Structures. 

Haloy, J.; Smith, W.W. 

NASA TH-83386, 1983. 

Perturbations to the Plasma Enviromnt 

Induced by the Orbiter's Maneuvering 

Thrusters. 

Murphy, G.B.; Shawhan, S.D.; Pickett, J.S. 

AIAA Paper 83-2599, 1983. 

Study of Auxiliary Propulsion Requirements 

for Large Space Stations. 

Smith, W.W.; Hackles, G.W. 

Executive Smry, vol. 1. NASA CR-168193, 

1983. 

Orbit-Raising and Maneuvering Propulsion - Research Status and Needs. 

Progress i n Astronautics and Aeronautics, 

vol. 89, Martin Smrfield, ed., American 

Institute of Aeronautics and Astronautics (New 

York, NY) , 1984. 

The Energetics of Hydrogen Atan 

Recabination - Analysis, Experiments, and 

Hodel ing. 

Filpus, J.W.; Hawley, H.C. 

17th International Electric Propulsion 

Conference Paper 84-77, 1984. 

Calculation of Vaporization Rates Assuning 

Various Rate Determining Steps: Application 

to the Resistojet. 

Hay, C.E. 

NASA TH-83757, 1984. 

Hydrazine and Its Derivatives - Preparation, 

Properties, -1 i cations. 

Schmidt, E.W. 

John Wiley & Sons, Inc. (New York), 1984. 

32 
Category 4 - Propel lent Management 

04:OOl: 1962 

04:002: 1962 

04:003: 1962 

04:004: 1962 

04:OO5: 1963 

04:006: 1964 

04:007: 1964 

04:008:1964 

Material Selection or Liquid Hydrogen Tank in 

the Arc Jet Feed System. 

Arthur 0. Little, Inc. NASA CR-96867, 1962. 

Propellant Storage and Transfer Systems for 

Electrothermal Engines. 

Barcley, R.B.; Singleton, A.H.; Stelts, P.D. 

Air Products and Chemicals, Inc. 

NASA CR-52157. 1962. 

Research and Development of Propellant Feed 

Systems for Ion Engines. 

Lawlor, P.J.; Montgomery, K.H. 

TRW-ER-5046 (NASA contract NAS-8-25251, 

Tharpson Rm Woolridge, Inc., 1962. 

Research and Development of Lithiun and 

Lithiun Hydride Propellant Feed Systems for 

Electric Propulsion Systems. 

Samuel, W.A.; Ciarlariello, T.A.; Shearer, R.E 

HSA Research Corp. (NASA contract NAS-8-25291, 

June 1962. 

Propellant Feed System for Electrothermal 

Engines. 

Wapato, P.G. 

Report SS-855-R (NASA contract no. NAS8-25721, 

Garrett Corporation Air Research Hfg. 

Division, Feb. 1963. 

Crogenic Propellant Feed Systems for 

Electrothermal Engines. 

Fwles, A.A. 

Arthur D. Little, Inc. NASA CR-60, May 1%4. 

Lithiun Feed Systems for Arc Jet Engines. 

Lawlor, P.J. 

TRW-ER-5444 (NASA Contract NAS3-25121, TRW 

Inc., Mar. 1964. 

Electrothermal Engine Propellant Storage and 

Feed System Study - Phase 11. 

Roos, G.E.; et al. 

Beach Aircraft Corp. NASA CR-52, 1964. 

04:009: 1970 

04:OlO: 1972 

04:011:1977 

04:012:1978 

04:013:1979 

04:014: 1979 

04:015:1981 

04:016: 1983 

The Development of Cryogenic Storage Systems 

for Space Flight. 

Davis, H.L.; Allgeier, R.K., Jr. 

NASA SP-247, 1970. 

Development of a Biwaste Resistojet 

Propulsion System Propellant Management and 

Control Subsystem. 

Greco, R.V.; Bliss, J.R.; Wilkenson, H.C. 

AIM Paper 72-448, Apr. 1972. 

Development and Qualification of the 

Propellant Management System for Viking 75 

Orbiter. 

Dowdy, H.W.; Hise, R.E.; Peterson, R.G. 

J. Spacecr., vol. 14, no. 3, Mar. 1977, 

p~. 133-140. 

Development and Qualification of the Space 

Shuttle Orbiter Reaction Control System 

Propellant Tank. 

Peterson, R.; Uney, P. 

AIM Paper 78-1026, July 1978. 

Cryogenic Storage System Development for Long 

Tern Space Missions. 

Anderson, J.E.; Eberhardt, R.N. 

AIM Paper 79-1261, June 1979. 

Performance of a Capillary Propellant 

Management Device with Hydrazine. 

Tegart, J.R. 

AIM Paper 79-1259, June 1979. 

Conceptual Design and Analysis of Orbital 

Crogenic Liquid Storage and Supply Systems. 

Eberhardt, R.N.; Cunnington, G.R.; Johns, W.A. 

Martin Marietta Corp. NASA CR-165321, 1981. 

Lw-Cost Titaniun Propellant Tankage. 

Leach, A.E.; Szpakwski, R.J. 

J. Spacecr., vol. 20, no. 6, Nov.-Dec. 1983, 

pp. 583-588. 

33 
Category 5 - Power and Control 

05:OOl: 1962 

05:002: 1962 

05:003: 1963 

05:004:1965 

05:005:1967 

05:006:1968 

05:007:1968 

05:008:1969 

05:009:1970 

05:010:1970 

05:011:1972 

Power Source for a 1 W Arc Engine Test 

Capsule. 

Boehme, R.; Cagle, G. 

ARS Preprint 3251-62, Pmerican Rocket Society, 

Mar. 1962. 

Parer Plant Consideration for an Arc Jet 

Space Propulsion System. 

Chen, H.H.; John, R.R.; Connors, J.F. 

Pmerican Rocket Society Space Powers 

Conference, Sept. 25-28, 1962, Santa Monica, CA 

Power Source for a 1 W Arc Engine Test 

Capsule. 

Boehme, R.J.; Cagle, E.H. 

AIAA J., vol. 1, no. 5, Hay 1963, 

pp. 1168-1169. 

Fuel Cells Using Storable Rocket Propellants. 

Athearn, L. 

Monsanto Research Corp. NASA CR-54640, 1965. 

HydrazineAiydrogen Peroxide Fuel Cell. 

Gruneberg , G. ; Weddel i ng , F . AFSC Conference, 1967, pp. 599-613. 

A Review of the Alkali Metal Rankine 

Technology Program. 

Hanson, S.V. 

J. Spacecr. Rockets, vol. 5, no. 11, 

Nov. 1968, p. 1124 

Rankine Cycle Systems Studies for Nuclear 

Space Power. 

Pitts, J.H.; Jester, H.H.L. 

Proc. 3rd IECEL, Aug. 1968. 

Study of a 300-Kilowatt Rankine Cycle 

Advanced Nuclear-Electric Space Power System. 

Heller, J.A.; kss, T.A.; Barna, G.J. 

NASA TH X-1919, 1969. 

Technology for Nuclear Electric Space Power 

English, R.E. 

Systems. 

NASA TM X-52771, 1970. 

Efficiency of Hydrazine-Peroxide Fuel Cells. 

Urbach, H.B.; Bwen, R.J. 

J. Electrochem. Soc., vol. 17, 1970, pp. 

1594-1600. 

Engineering Aspects of Hydrazi ne-Ai r Fuel 

Cell Power Systems. 

Andrew, H.R. 

J. Appl. Electrochem., vol. 2, 1972, pp. 

327-336. 

05:012: 1972 

05:013:1972 

05:014: 1973 

05:015:1973 

05:016: 1973 

05:017:1975 

05:018: 1975 

05:019:1976 

05:020: 1978 

05:021:1979 

State of Development of Hydrazine Fuel Cells, 

Their Problems and Potential Technical 

Appl i cati ons. 

Gutjar, H.A. 

In: 

Batelle Seattle Research Center, G. Sandstede, 

ed., University of Washington Press, 1972, 

Fran Electrocatalysis to Fuel Cells, 

pp. 143-156. 

Optimizing Power Efficiency of Hydrazine 

Oxygen Fuel Cells. 

Urbach, H.B. 

In: 

Publications Carmittee, 1972, pp. 182-185. 

25th Annual Power Sources Symposium PSC 

Interface Requirements for Electric 

Propulsion Power Processing Equipment. 

Biess, J.J.; Schoenfield, A.D.; Goldin, D.S. 

AIAA Paper 73-1108, 1973. 

Battery-Powered Electric Propulsion for 

North-South Stationkeepi ng . Free, 8.; Dunlop, J. 

COMSAT Tech. Rev., vol. 3, no. 1, Spring 1973. 

High Power Density Hydrazine Fuel Cells. 

Icenhower, D.E.; Urbach, H.B. 

8th Intersociety Energy Conversion Engineering 

Conference, Paper 739009, 1973, pp. 67-71. 

Exxon Parer Cell. 

Ocean Industry, July 1975, p. 46. 

Electrochemical Cell Suitable for Operating 

in All Positions. 

Hespel, C. 

U.S. Patent 3902919, Nov. 14, 1973/Sept. 2, 

1975. 

Exhaust Gas Carpositions and Fuel 

Efficiencies of Hydrazine-Air Fuel Cells. 

Tarmra, K.; Kahara, T. 

J. Electrochem. SOC., vol. 23, 1976, pp. 

7 76-780. 

Solar Array Systems - Future Orbital Power 

Systems Technology Requirements. 

Crabtree, W.L. 

NASA CP-2058, 1978, pp. 147-155. 

Study of Reactor Brayton Power Systems for 

Nuclear Electric Spacecraft. 

Harper, A. 

NASA CR-168942, 1979. 

34 
05:022:1979 Nuclear Electric Power System for Solar 

System Exploration. 

Philips, W.H. 

AIM Paper 79-1337R, June 1979. 

05:023: 1980 Reactor/Brayton Power Systems for Nuclear 

Electric Spacecraft. 

Layton, P. 

Proc. 15th IECEC, AIM (New York), Aug. 1980, 

p. 732. 

05:024: 1981 Reactors for Nuclear Electric Propulsion. 

Buden, D.; Angelo, J.A. 

AIM Paper 81-0697, Apr. 1981. 

05:025: 1982 Power Generation fm Nuclear Reactors in 

Aerospace Applications. 

English, R.W. 

NASA TH-83342, 1982. 

05:026:1982 The Liquid Droplet Radiator - An Ultralight 

Heat Rejection System for Efficient Energy 

Conversion in Space. 

Hattick, A.T.; Hertzberg, A. 

Acta Astronaut., vol. 9, no. 3, 1982, 

pp. 165-172. 

05:027:1983 Evaluation of the Use of On-Board Spacecraft 

Energy Storage for Electric Propulsion 

Nissions. 

Poeschel, R.L. 

Hughes Research Laboratories. NASA CR-168209, 

1983. 

05:028: 1984 Satellite Reaction Control Subsystem with 

Augnented Catalytic Thrusters. 

Feconda, R.T.; Weimn, J.I. 

AIM Paper 84-1235, June 1984. 

05:029:1984 The Status of Parer Supplies for Primary 

Electric Propulsion in the USA. 

Jones, R.H.; Scott-Honck, J.A. 

17th International Electric Propulsion 

Conference, IEPC Paper 84-83, 1984. 

35 
category 6 - Pulsed Electrothermal Engines 

06:OOl: 1982 Theory of the Pulsed Electrothermal Thruster. 

Burton, R.L.; Goldstein, A.; Tihan, D.A.; 

Winsor, N.K. 

AIAA Paper 82-1952, Nov. 1982. 

06:002: 1983 Investigation of a Pulsed Electrothermal 

Thruster. 

Burton, R.L.; Goldstein, S.A.; Hilko, B.K.; 

Tichn, D.A.; Winsor, N.K. 

GT-Devices, Inc. NASA CR-168266, 1983. 

36 

06:003: 1984 Experimental Investigation of the Pulsed 

Electrothermal (PET) Thruster. 

Burton, R.L.; Goldstein, S.A.; Hilko, B.K.; 

Tihan, D.A.; Winsor, N.K. 

AIAA Paper 84-1386, June 1984. i 

06:004:1984 Proposed System Design for a 20 kw Pulsed I 

Electrothermal Thruster. 

Burton, R.L.; Goldstein, S.A.; Hilko, B.K.; 

Tihan, D.A.; Winsor, N.K. 

AIM Paper 84-1387, June 1984. 

I 

I 

I 

1 
Category 7 - RF and Microwave Devices 

07:001:1961 The Induction Coupled Plasma Torch. 

Reed, T.B. 

J. Appl. Phys., vol. 32, no. 5, Hay 1961. 

07:002:1969 Parametric Design of High Frequency 

Propulsion Systems for Tests in Space. 

Freisinger, J.; Loeb, H.W. 

DGLR-69-022, Giessen Univ., Hay 1969 (in 

German). 

07:OO3: 1971 High-Density Resonantly Sustained Plasm in 

a Variable-Length Cylindrical Cavity. 

Fredericks, R.H.; Awnussen, J. 

Appl. Phys. Ltr., vol. 19, 1971, pp. 508-510. 

07:004:1974 The Design of a Hicrcuave Plasma Cavity. 

Awnussen, J.; Hallavarpu, R.; Hwrann, J.R.; 

Park, H.C. 

Proc. IEEE, vol. 62, Jan. 1974, pp. 109-117 

07:005: 1974 The Induction Arc: A State-of-thedrt 

Review. 

Eckert, H.U. 

High Temp. Sci., vol. 6, 1974, pp. 99-134. 

07:006:1978 Behavior of a Hicrcuave Cavity Discharge 

over a Wide Range of Pressures and Flow 

Rates. 

Hallavarpu, R.; Awnussen, J.; Hawley, H.C. 

IEEE Trans. Plasm Sciences, vol. 4, PS-6, 

D~C. 1978, pp. 341-354. 

07:OO7: 1981 Free Radical Propulsion Concept. 

Hawkins, C.E.; Nakanishi, S. 

NASA TH-81770, also AIM Paper 81-0676, 1981. 

07:008: 1981 Atanic Hydrogen Rocket Engine. 

Etters, R.P. and Flurchick, K. 

AIM Paper 81-0677, 1981 

07:009: 1982 Measurements of Energy Distribution and 

Thrust Energy to Hydrogen for Propulsion. 

Ilorin, T.; Chapman, R.; Filpus, J.; 

Hawley, H.; Kerber, R.; Awnussen, J.; 

Nakanishi, S. 

AIM Paper 82-1951, Nov. 1982. 

37 

07:010:1982 

07:011:1984 

07:012: 1984 

07:013:1984 

Oi:Oi4:i984 

07:015: 1984 

Standing Waves Along a Hicrowave Generated 

Surface Wave Plasma. 

Rogers, J.; Asmussen, J. 

IEEE Trans. Plasma Science, vol. PS-10, Hat-. 

1982, p~. 11-16. 

heasurements of Energy Distribution in 

Hicrowve Plasmas of N2 and He and 

Caparisons with Results for H2. 

Chapman, R.; Hawley, H.C. 

In: 17th International Electric Propulsion 

Conference, IEPC 84-76, Japan Society for 

Aeronautical and Space Sciences, Tokyo, 1984. 

Prospects for nicrarave Heated Propulsion. 

Hicci, H.H. 

AIM Paper 84-1390, 1984. 

Time Dependent Solution of the Fully Coupled 

Boltmnn and llacroscopic Balance Equations 

for a Two Conponent Self-Sustained Microwave 

P1 asma. 

Norin, T.J.; Hawley, H.C. 

17th International Electric Propulsion 

Conference, IEPC 84-75, 1984. 

knmstratior! of a New E!ectrothermal 

Thruster Concept. 

Whitehair, 5.; Awnussen, J.; Nakanishi, 5. 

Appl. Phys. Ltr., Hay 1984. 

Experiments with a Microwave Electrothermal 

Thruster Concept. 

Whitehair, S.; Asmussen, J.; Nakanishi, S. 

17th International Electric Propulsion 

Conference, IEPC 84-74, 1984. 
Category 8 - Solar Thermal Thrusters 

08:OOl: 1979 Solar Rocket System Concept Analysis. 08:003: 1983 Performance Potential of Advanced Solar 

Etheridge, F.G. Thermal Propulsion. 

AFRPL-TR-79-79, NOV. 1979. Shoji, J.H. 

08:002:1979 A New Solar Thermal Receiver Utilizing a 

Small Practice Heat Exchanger. 

Hunt, A.J. 

14th Intersociety Energy Conversion 

Engineering Conference, Aug. 1979. 

AIM Paper 83-1307, June 1983. 

38 
09:OOl: 1972 

09:OO2: 1972 

09:003:1972 

09:004: 1974 

09:OO5: 1975 

uY;vM. I7fU 

09:007: 1976 

09:008: 1976 

09:009: 1976 

09:010:1977 

09:011:1978 

Category 9 - Laser Thermal Propulsion 

Propulsion to Orbit by Ground Based Lasers. 

Kantrowi tz, A. 

Astronaut. and Aeronaut., vol. 10, no. 5, May 

1972, p. 74. 

Laser Propulsion. 

Pirri, A.N.; Weiss, R.F. 

AIAA Paper 72-719, June 1972. 

Laser Propulsion. 

Ran, R.E.; Putre, H.A. 

NASA TM X-2510, 1972. 

Propulsion by Absorption of Laser Radiation. 

Pirri, A.N.; Monsler, M.J.; Nebolsine, P.E. 

AIAA J., vol. 12, no. 9, Sept. 1974, 

p~. 1254-1261. 

Radiant Energy Absorption Studies for Laser 

Propulsion. 

Caledonia, G.E.; Wu, P.K.S.; Pirri, A.N. 

NASA CR-134809. 1975. 

Laxi ,,;.--.lpt Engine. 

Barchukov, A.I.; Bunkin, F.V.; Konov, V.I.; 

Prokhorov, A.M. 

JETP Ltr., vol. 23, no. 5, Mar. 1976, 

pp. 213-215. 

Uses of a Laser Energy Source in Producing a 

Reactive Thrust. 

Bunkin, F.V.; Prokhorov, A.M. 

Soviet Physics - Uspekhi, vol. 19, no. 7, July 

1976, pp. 561-573. 

Investigation of Beamed Energy Concepts for 

Propulsion. Volune 1. 

Huberman, M. ; et al. 

AFRPL-TR-76-66, Oct. 1976. 

Laser Heated Rocket Studies. 

Kenp. N.H.; Root, R.G.; Wu, P.K.S.; 

Caledonia, G.E.; Pirri, A.N. 

NASA CR-135127, 1976. 

The Fluid Mechanics of Pulsed Laser 

Propul si on. 

Simons, G.A.; Pirri, A.N. 

AIAA J., vol. 15, no. 6, June 1977, 

pp. 835-840. 

CW Laser Propulsion. 

Legner, H.H.; Douglas-Hamilton, D.H. 

J. Energy, vol. 2, Mar.-Apr. 1978, pp. 85-94. 

09:012: 1980 

O9:013: 1980 

09:014:1980 

09:015:1981 

09:016: 1981 

09:017:1981 

09:018:1982 

09:019: 1982 

09:020:1982 

09:021:1983 

Laser Propulsion - 1980. 

Jones, L.W. 

AIAA Paper 80-1264, 1980. 

Laser Heated Thruster - Interim Report. 

Kenp, N.H.; Lewis, P.G. 

NASA CR-161665, 1980. 

Laser Heated Thruster. 

Kenp, N.H.; Krech, R.H. 

NASA CR-161666, 1980. 

Measured Molecular Absorptivities for a 

Laser Thruster. 

Fowler, M.C. 

AIM J., vol. 19, no. 8, Aug. 1981, 

p~. 1009-1014. 

Simplified Models of CW Laser-Heated 

Thrusters. 

Kenp, N.H. 

AIM Paper 81-1249, June 1981. 

Pulsed Laser Propulsion. 

Nebolsine, P.E.; Pirri, A.N.; Goela, J.S.; 

Simons, G.A. 

AIAA J., vol. 19, no. 1, Jan. 1981, 

pp. 127-128. 

Study of Laser Heated Propulsion Devices, 

Part I. 

Hofer, O.C.; Thoenes, J. 

LMSC-HREC-TR-D784744, Apr. 1982. 

NASA's Laser-Propulsion Project. 

Jones, L.W.; Keefer, D.R. 

Astronaut. Aeronaut., vol. 20, no. 9, Sept. 

1982, pp. 66-73. 

A Two-Dimensional Model of the Hydrogen 

Plasma for a Laser Powered Rocket. 

Keefer, D.R. ; Crowder, H. ; El kins, R. 

AIAA Paper 82-0404, Jan. 1982. 

Orbit Raising and Maneuvering 

Propulsion - Research Status and Needs. 

Caveny, L.H., ed. 

Progr. Astronaut. Aeronaut., vol. 89, 1983. 

39 
09:022: 1983 A NASA High-Parer Space-Based Laser Research 09:024: 1984 Laser Propulsion. 

and Applications Program. 

DeYoung, R.J.; Walberg, G.D. ; Conway, E. J. ; 

Jones, L.W. 

NASA SF-464, 1983. 

Kenp, N.H.; Rosen, D.I. 

AIM Paper 84-1445, June 1984. 

09:025: 1984 muter Simulation of the Non-Steady Flw 

of a Real Gas with Laser Energy Absorption. 

09:023:1984 A Two-Dimensional Analysis of Laser Heat Kenp, N.H. 

Addition in Converging Nozzles. AIM Paper 84-1569, 1984. 

AIM Paper 84-0529, 1984. 

40 
AUTHOR INDEX 

Pbbott, E. 3:149 

Abe, J.T. 1:123 

Adachi, K. 2:146 

Adcock, B.D. 2:59 

Albert, H.J. 1:124 

Allen, K. 1:164 

Allgeier, R.K., Jr. 4:9 

Alt, R.E. 3:179, 3:183 

mur, I. 3:7 

Anderson, J.E. 4:13 

Andrew, H.P. 5:11 

Angelo, J.A. 5:24 

Anselmi, R.T. 3:156 

Antoine, A.C. 3:55 

Arthur, P.D. 1:160, 2:70 

Awnussen, J. 7:3, 7:4, 7:6, 7:9, 

Athearn, L. 5:4 

7:10, 7:14, 7:15 

Babet, G.I. 3:l 

Back, L.H. 3:56, 3:106, 3:llO. 3:124 

Bade, W.L. 2:23, 2:52, 2:63 

Baerwald, R.K. 3:166 

Baiiey, A.G. 3:i25 

Baldwin, L.V. 3:15 

Balzer, D.L. 3:140 

Banks, B.A. 3:135, 3:150 

Barber, A.J. 1:211 

Barber, B.C. 3:141, 3:145, 3:167 

Barberis, N.J. 3:200 

Barchukov, A.I. 9:6 

Barcley, R.B. 4:2 

Barker, F.C. 3:175, 3:180 

Barna, G.J. 5:8 

Barrett, C.C. 1:50 

Barter, A.J. 1:209 

Bassichis, J. 3:152 

Batson, J.L. 3:102 

Baty, R. 1:162, 3:127 

Bauermeister, K.E. 3:29 

Beckmann, H. 3:30 

Belsley, A.C. 3:140 

Bender, R.W. 2:53 

Bennett, S. 1:12, 1:13, 1:21, 

1:22, 1:35, 1:36, 2:54, 2:62, 

2~65-67, 2: 106 

Berkopec, F.O. 3:73 

Bertolo, C.V. 2:117, 2:131, 2:132 

Biess, 3.5. 5:14 

Bird, K.O. 3:31 

Birkebak, R.C. 2: 118 

Bjorkland, R.A. 3: 143 

Bliss, J.R. 1:95, 1:125, 1:126, 

1:155, 1:156, 4:lO 

Boehme, R. 5:1, 5:3 

Bond, A. 3:146 

Boucher, R.A. 2:82, 3:51 

Bowen, F. 3:57 

Wen, R.J. 5:lO 

Wry, A. 3:176 

Braitinger, H. 1:213 

Bray, K.N.C. 3:9 

Breves, E.O. 3:187 

Bright, A.W. 1:175 

Brockman, P. 3:57 

Brogan, T.R. 3:lO 

Br-rs, H.L. 1:9 

Brown, C.T. 3:158 

Bruun, E.R. 1:176, 1:220, 1:224 

Bryant, W.A. 3:168 

Bryson, R.J. 2:108 

Buden, D. 5:24 

Buhler, R.D. 2:17, 2:55, 2:83, 2:90 

Bunkin, F.V. 9:6, 9:7 

Burhorn, F. 3:16, 3:17 

Burton, R.L. 6:l-4 

Butler, D.S. 3:32 

Byers, 0. 1:239, 3:181 

Byke, R.H. 1:61-63 

- -_ PUIII~, n., . .I.-, 

Cagle, E.H. 5:3 

Cagle, G. 5:l 

Caledonia, G.E. 9:5, 9:9 

Callens, R.A. 1:84, 1:93, 1:148, 1:207 

Cann, G.L. 

Carlson, R.A. 1:221 

Carre, D.J. 3:198 

Carter, F.V. 3:29 

Cassanova, R.A. 3:58 

Caveny, L.H. 9:21 

Chanpion, K.S.W. 2:5 

Chandler, W.T. 3: 169 

Chapin, S.G. 1:85 

Chapman, A.J. 3:30 

Chapman, R. 7:9, 7:11 

Charhut, D.E. 1:86 

Chen, H.H. 

2:63, 2:66, 5:2 

Chirivella, J.E. 3:151 

Chubb, W.B. 3:111 

Ciarlariello, T.A. 4:4 

Clark, J.P. 3:194 

Clark, K.E. 1:12, 1:156. 1:188, 

1:199, 2:131 

Wine, J.D. 3:8 

Cochran, A.A. 3:81 

2:9, 2:55, 2:83, 2:89, 

2:102, 2:121, 2:125, 2:140 

2:21, 2:34, 2135, 2:40, 

Cochran, T. 1:230 

Cohen, F. 1:127 

Connoly, D.J. 3:85, 3:89, 3:97 

Connors, J.F. 

Conway, E.J. 9:22 

Cooper, K.C. 3:126 

Crabtree, W.L. 5:20 

Cremers, C. 2:103, 2:118, 2:124, 3:103 

Crespo, A. 1:130, 3:112, 3:120 

Crosswy, F.L. 3:74 

Crcuder, H. 9:20 

Cuffel, R.F. 3:110, 3:124 

Cmbers, L. 1:9 

Cunnington, N.R. 4: 15 

Cutler, W. 3:75 

Cygnarowicz, T.A. 1:51, 1:52, 1:64 

Czika, J., Jr. 2:106 

l:lO, 2:21, 2:22, 2:35, 

2:40, 2:62, 2:65-67, 5:2 

Davis, O.D. 2:43 

Davis, H.L. 4:9 

1:204, 1:211 

Dazzo, J.J. 3:64 

Debolt, H. 2:63, 2:64 

Deissler, R.G. 3:18 

Delcroix, J.L. 2:137 

Demetriades, S.T. 3:23 

Dennis, T. 3:119 

Desai, J.D. 3:178 

DeWeiss, F.A. 2:51 

DeYoung, R.J. 9:22 

Dixon, J.C. 1:149, 3:142 

Danitz, S. 2:56 

Donaldson, J.F. 3:81 

Donovan, J.A. 1:96, 1:109, 1:150, 

1:164, 1:177, 1:187 

Donovan, R.H. 1:240 

Douglas-Hamilton, D.H. 9:11 

Dowdy, H.H. 4:11 

Oressler, G.A. 1:225 

Oucati, A.C. 1:12, 1:13, 1:24, 1:88, 

Ouckett, R.J. 2:128 

Duncan, L.F. 1:097-101 

Dunlop, J. 5:15 

Dunnill , W.A. 2: 110 

n-..:- 1.1 t 1.07 1.a~ i.iac, 1.7n1 

2:9, 2:84, 2:85, 2:109 

Earl, A.C. 1:100, 1:151 

Eberhardt, R.N. 4:13 

Ecker, G. 2:19, 2:141 

Eckert, E.R.G. 2:46, 2:90, 2:104, 

2:116, 2:122 

Eckert, H.V. 7:5 

41 
Eddy, 1. 2:104 

Edwards, I. 1:138, 1:152, 1:153, 

1:182, 1:189 

Ehlers, J.G. 3:46 

Ehricke, A. 2:lO 

Elkins, R. 9:20 

Emnons, O.L. 1:227, 3:168 

Endres, D.L. 3:76 

English, R.E. 5:09, 5:25 

Enos, G.R. 1:lOl. 1:114, 1:129, 1:143 

Ernstene, H.P. 1:37 

Eschenroeder, A.Q. 3: 19 

Esker, D.W. 2:114 

Etheridge, F.G. 3:177, 8:l 

Etters, R.P. 7:8 

Eusanio, E. 1:53, 1:65, 1:66 

Fabri, J. 1:38 

Fearn, D.G. 1:188, 1:200, 1:226, 3:191 

Feconda, R.T. 5:28 

Ferguson, H. 1~54, 1:67 

Ferrante. J. 1:18, 2:91, 3:54 

Ferreira, C.H. 2: 137 

Filpus, J.W. 3:206, 7:9 

Finke, R.C. 1:178, 3:59 

Finkelnberg, W. 2:6, 2:38 

Finston, R. 1:217, 3:188, 3:192 

Flurchick, K. 7:8 

Forbes, S.G. 1:68 

Fowler, H.C. 9:15 

Fowles, A.A. 2:57, 4:6 

Fradkin, D.B. 2:111, 3:132 

Fraga, E. 1:130, 3:112, 3:120 

Frazine, O.F. 3:183 

Fredericks, R.H. 7:3 

Free, B.A. 1:102, 2:42, 5:15 

Freisinger, J. 7:2 

French, J.B. 3:24 

Fritz, O.E. 1:218, 1:225, 3:152 

Frohlick, J.P. 2:lW 

Fryburg, G.C. 3:14 

Gallagher, R.L. 2:89, 2:102, 2:123 

Gardner, W.N. 3:78 

Garfinfel, H. 

Gardner, W.N. 3:77 

Garrison, P.W. 3: 199 

Gates, D.W. 2:36, 2:37 

Gaubatz, W.A. 1:131 

Geideman, W.A. 2:24, 2:73 

Gerhard, H. 2:16 

Ghei, H.L. 2:lOO 

Ghosh, R. 1:89 

Giannini, G.H. 1:88, 2:85 

Gibbs, T.W. 2:63 

Gibson, R.N., Jr. 1:51, 1:52, 1:64 

Gier, H.L. 3:56 

3: 162, 3: 184 

Gilberg, L.A. 2:119 

Girovard, H. 3:44 

Goela, J.S. 9:17 

Goldin, D.S. 5:14 

Goldstein, S.A. 6:l-4 

Good, R.H., Jr. 2:7 

Goodnan, H. 1:39, 1:55, 1:103, 1:163 

Gordon, 5. 3:46 

Grabbi, R. 1:154, 1:180, 1:206, 

1:212, 3:159 

Graber, F.H. 3:44 

Graves, R. 2:133 

Greco, R.V. 1:61-63, 1:69-71, 1:81, 

1:86, 1:90, 1:95, 1:123, 1:125, 

1:126, 1:132, 1:155, 1:156, 2:39, 

2:58, 4:lO 

Greenspan, H.P. 3:32 

Greer, H. 3:65, 3:78 

Grey, J. 2:111, 3:33 

Griep, O.J. 3:78 

Grier, N.T. 3:34 

Grishin, S.D. 3:153 

Gruneberg, G. 5:5 

Gutjer, H.A. 5:12 

Halbach, C.R. 1:40, 1:47, 1:72, 

1~91, 1:104-106, 1:118, 1:119* 

1 : 133-136, 1~43, 1: 157-161, 1: 163, 

3: 131 

Hall, C.A. 3:134 

Hall, C.E. 3:64 

Hall, D.F. 3:198 

Hall, J.G. 3:19 

Hamann, J.B. 7:4 

Hannum, N.B. 1:240 

Harden, D.G. 3:61 

Harder, R.L. 2:83, 2:121, 2:125 

Hardy, T.L. 2:144 

Harp, J.L., Jr. 3:42 

Harper, A. 5:21 

Harvey, J.K. 2:59 

Hassan, H.A. 2:126, 2:129 

Havell, R.F. 3:60 

Hawk, C. 1: 162, 3: 125 

Hawkins, C.E. 7:l 

Hawley, H.C. 3:206, 7:6, 7:9, 7:11, 

Haws, J.L. 3:61 

Hayman, C. 3:176 

Hayn, 0. 1:213, 3:171 

Hazelrigg, G.A., Jr. 3:82 

Heimel, 5. 3:46 

Heller, G.B. 

Hermann, H. 2:64 

Hernquist, K.G. 2:12 

Hertzberg, A. 5:26 

Hespel, C. 5:18 

7: 13 

2:11, 2:20, 3:35, 5:8 

Hess, R. 3:56 

Hilko, B.K. 6:2-4 

Hill, C.S. 1:105, 1:106, 1:118, 

Hill, J.S. 1:124 

Hise, R.E. 4:11 

Hoeber, C.F. 3:200 

Hoercher, H.E. 2:21, 2:63 

Hoertel, F.W. 3:81 

Hofer, O.C. 9:18 

Hogan, W. 2:64 

Holccnh, L.B. 3:113, 3:128 

Holdaway, R. 1:179, 3:129 

Holm, R. 2:3 

Holmes, A.D. 3:59 

Holtz, F.C. 3:60 

Honig, R.E. 3:6 

Horn, D.D. 2:140 

Hosack, G.A. 3:114 

Hoskstra, P.D. 3:27 

Howard, J.H. 1:3, 1:4, 3:47 

Huberman, H. 9:8 

Hudson, G. 1:89, 1:230 

Hwrpel, H. 2:60, 2:75 

Hunczak, H.R. 1:87 

Hunt, A.J. 8:l 

Hunter, C.R. 1:166 

Huss, W. 1:21 

1:119, 1:134, 1:144 

Iakovlev, E.A. 3:193 

Icenhower, D.E. 5:16 

Isley, W.C. 1:73-75 

Jack, J.R. 1:1, 1:2, 1:5, l:lO, 1:16, 

Jackson, B. 1:237, 1:238, 2:55, 3:75 

Jackson, F.A. 1:41 

Jacobs, P.F. 3:33 

Jaffe, L.D. 3:26 

Jahn, R.S. 2:109, 2:135 

James, J.P. 2:86 

James, N.E. 1:131 

Jansson, R.E.W. 1:128, 1:153, 1:179, 

1:182, 1:189, 3:129 

Jarrett, 0. 3:57 

Jeffries, N.P. 1:9, 1:17 

Jester, H.H.L. 5:7 

John, R.R. 1:11, 1:21, 1:22, 1:25-27, 

1:23, 1:29, 2:61, 3:25 

1~35, 1:36, 1~42-44, 2~21-23, 2~35, 

2~40, 2141, 2:51, 2:62-69, 2~87, 

2:101, 2:107, 5:2 

Johns, W.A. 4:15 

Jonath, A.D. 3:62, 3:63 

Jones, L.W. 3:172, 9:12, 9:19, 9:22 

Jones, R.H. 3:201, 5:29 

42 
Kahura, T. 5:19 

Kalb, H.T. 3:74 

Kallis, J.H. 1:163 

Kanning, G. 3:66 

Kantrouitz, A. 9:l 

Kaplan, D.I. 3:201 

Kato, T. 2:142 

Kaufman, H. 2:120 

Keefer. D.R. 9:19, 9:20 

Keller, T.A. 3:59 

Kelly, A.J. 1:156 

Kenp, N.H. 

9:24, 9:25 

Kent, P.J.C. 3:176 

Kerber, R. 7:9 

Kerr, G.P. 2:42 

Keyte, G.E. 1:210 

King, C.R. 3:20 

Kingsley, T.C. 1:176, 1:224 

Klein, J.J. 3:19 

Klemetson, R.W. 3:199 

Kohl, W.H. 3:79 

Koneval, D. 3:14 

Konov, V.I. 9:6 

Korder, R.L. 2:89 

Koslov, N.P. 3:153 

Kosson, R.L. 1:45, 2:96 

Krause, S. 2:127 

Krech, R.H. 9:14 

Krieser, F.J. 3:11, 3:12 

Krieve, W.P. 1:107 

Krishman, H. 2:135 

Kuenzly, J.D. 1: 180, 1: 190-192, 

Kuluva, N.H. 3:114 

Kurzhals, P.R. 1:76 

Kusko, A. 2:64 

Lame, H. 3:182 

Lafferty, J.H. 2:4 

Landis, F. 3:36 

Landsbaum, E.H. 3:13 

Larson, V.R. 3:164 

Laubach, G.E. 1:097, 1:099 

Laville, H. 1:137 

Lawlor, P.J. 4:3. 4:7 

Layton, P. 5:23 

Lazar, J. 1:181 

Leach, A.E. 4:16 

Lecoq, H. 1:219 

Lee, T.H. 2:13, 2:15 

Legner, H.H. 9:11 

LeGrives, E. 1:38 

Leon, H.I. 3:90 

Leskov, L.V. 3:153 

Lester, J.T. 1:223 

Levitt, L. 3:38 

9:9, 9:13, 9:14, 9:16, 

1:207, 1:221, 1:222 

Leuellen, W. 3:68 

Leuin, R. 1:182 

Leuis, P.G. 9:13 

Liebermann, R. 2:66, 2:64 

Lindgren, J.R. 3:52 

Loeb, H.W. 3:105, 3:147, 7:2 

Lord, W.T. 1:96, 1:108-110, 

Lund, W. 1:77, 1:87 

Luquet, P. 1:111 

Lynch, R.A. 3:130, 3:141 

1:150, 1:164, 1:165, 1:177, 1:193 

Mackeown, S.S. 2:l 

Hackles, G.W. 3:204 

Placklis, H. 1:214, 1:218 

bcs, H.E. 3:70 

Hacomber, H. 2:22, 2:44, 2:74 

Haecker, H. 2:6, 2:38 

bhan, J.R. 2:124, 3:103 

Makin, B. 1:175 

Hallavarpu, R. 7:4, 7:6 

Malou, J. 3:202 

Hanson, S.V. 5:6 

Haqueet, J. 1:219 

Marble, E. 3:45 

Marchand, F.E. 2:70, 2:71 

Marcisz, T.J. 1146 

Marion, C. 1:79, 1:92 

brlotte, G.L. 2:55, 2:121 

Martinek, F. 2:24 

Mason, E.A. 3:7 

bsser, P.S. 

Massey, H.S.W. 3:2 

Massier, P.F. 3:56, 3:106, 3:124 

Hattick, A.J. 5:26 

May, C.E. 3:14, 3:27, 3:207 

Mayo, R.F. 2:43 

HcBride, B.D. 3:46 

HcCaughey, O.J. 1:159, 2:70, 2:71, 

HcGee, H.A. 3:35 

HcHush, D. 3:119 

HcKenna, Q.H. 2:36 

HcKevitt, f .X. 1:234, 1:241 

Heese, R.A. 1:217 

Meetin, R.J. 3:148 

Hegrue, J. 2:40, 2:65 

Hicci, H.H. 7:12 

Hickelsen, W.R. 1:56, 1:57, 1:73, 

HigQ1, D. 3:36 

Hiller, H.C. 2:136 

Hilligan, H.W. 3:53 

Hills, R.G. 3:52 

Hironer, A. 2:22, 2:44, 2:74 

Hirtich, H.J. 1:231 

2:17, 2:25, 2:29, 2:72, 

2: 145 

2:73, 2:88 

1:75, 1:79, 3:90, 3:91 

Hiyake, C.I. 1:243 

Molitor, J.H. 1:235 

Honsler, H.J. 9:4 

Montgomery, K.H. 4:3 

Moore, R.A. 

Morgan, D. 1:25 

Morin, R. 1:78, 1:92, 3:107 

Morin, T.J. 7:9, 7:13 

Morningstar, R.E. 1:225 

Morris, J.C. 2:130 

Moss, T.A. 5:8 

Moynihan, P.I. 3:143 

Huehlberser, E. 1:14, 1:15, 1:24, 

1:88, 2:85, 2:109 

Huenzer, F.B. 1:138 

Huller, K. 2:73 

Hullin, J.P. 3:92 

Hunoz, A. 3:120 

Hurch, C.K. 1:46, 1:107, 1:127, 

2:55, 2:83, 2:89, 2:102 

1:148, 1:156, 1:166, 1:167, 1:178, 

1:183, 1:184, 1:194, 1:206, 1:207, 

1:212, 3:84 

Murphy, E.L. 2:7 

Murphy, G.B. 3:203 

Murphy, S.N.B. 2:94 

Husgrove, P.J. 1:149. 3:143 

Eyers, B.F. 3:44 

Nakanishi, S. 2:144, 7:7, 7:9, 7:14, 

Nebolsine, P.E. 9:4, 9:17 

Nelson, W.G. 1:95 

Neurath, P. 2:62 

Newton, N.C. 3:148 

Noel, H.B. 3:106 

Norton, D.J. 3:144 

7: 15 

Oconnor, T.J. 1:201, 1:211, 3:158 

Oggero, H.V. 2:45, 2:117, 2:131, 

2:132, 2:134 

Ohtsuka, H. 2:143 

Olson, W.L. 3:37 

Oswalt, L.R. 3:42 

Owens, W.L., Jr. 1:138, 3:115 

Ownby, H.L. 1:91 

Page, R.J. 1:6, 1:7, 1:28, 1:40. 

1~47, 1~58, 1~69-71, 1:80, 1~81, 

1:91, 1:106, 1:112, 1:118, 1:131. 

1:140, 1:158-160, 1:232, 2:16, 2:17, 

2:60, 2:74 

Park, H.C. 7:4 

Parkinson, R.C. 1:108, 1:110, 1:164 

Passemaneck, R.S. 3: 166 

Pawlick, E. 1:230 

Pegot, E.B. 2:115 

1 : 202 

43 
Pekar, P.P. 2:154 

Pena, N.A. 2:lOO 

Perlmutter, M. 3:18 

Peterson, R.E. 2:145 

Peterson, R.G. 4:11, 4:12 

Pfeffer, H.A. 3:155, 3:159 

Pfeifer, G.R. 1:168 

Pfender, E. 

Pharo, T.J. 3:134 

Philips, W.M. 5:22 

Phillips, D.G. 1:141, 1:169, 1:170 

Pickett, J.S. 3:203 

Pirri, A.N. 9:2, 9:4, 9:5, 9:9, 9:10 

Pisciotta, A., Jr. 1:48, 1:53, 1:61, 

Pitts, J.H. 5:7 

Poeschel, R.L. 5:27 

Proeschel, R.A. 1:098 

Prokhorov, A.M. 9:6, 9:7 

Pusmire, T.K. 1:59, 1:77, 1:84, 1:85, 

1:87, 1:93, 1:94, l:lOl, 1:113, 

1:114, 1:129, 1:142, 1:143, 1:195, 

1:194, 1:203, 1:211, 1:214, 2:099, 

3: 160 

2:90, 2:103, 2:104, 2:116, 

2:132, 2:138 

9: 17 

1;62, 1:65, 1:66, 1:82, 3:67 

Putre, H.A. 9:3 

Quick, J. 1:162, 3:127 

Rae, W.J. 3:117 

Ragent, B. 3:39 

Raheli, F. 3:106 

Rawlin, V. 3:150 

Reed, T.B. 7:Ol 

Reid, J.W. 2:26 

Rendleman, J.D. 1:223 

Rich, J.A. 2:27 

Richards, R.E. 3:161 

Richardson, N.K. 1: 185 

Richter, R. 2:76, 2:77, 2:81 

Robotti, A.C. 2:45 

Robson, A.E. 2:8 

Roehling, D.J. 3:132 

Rogers, J. 7:lO 

Rollbuhler, R.J. 3:94 

Ran, F.E. 9:3 

Rms, G.E. 4:8 

Root, R.G. 9:9 

Rosen. D.I. 9:24 

Rosenbam, B.M. 3:38 

Rothe, D.E. 3:108, 3:118 

Rott, N. 3:68 

Roux, J.A. 3:183 

Rudey, C. 1:221 

Rudin, M. 3:39 

Runavot, M. 3:182 

Runstadler. P.W. 2: 112 

Sabol, A.P. 2:128 

Sackheim, R.L. 1:207, 1:214, 1:218, 

1:225, 3:152 

Saito, K. 2:79 

Saltz, L.E. 1:227 

Samuel, W.A. 4:4 

Sandboro, V.A. 3:15 

Sanservero, V.J., Jr. 3:87, 3:162, 

Savage, A. 1:96, 1:109 

Schaedle, D.C. 1:098 

Schaefer, J.W. 1:18, 2:61, 2:91, 

Schlicting, H. 3:21 

Schmidt, E.W. 3:208 

Schmitz, H. 1:171, 1:204, 1:228 

Schrmcker, R.H. 1:213, 3:172 

Schoeck, P.A. 2:46, 2:92 

Schoenfield, A.D. 5: 14 

Schreib, R.R. 1:85, 3:163, 3:175, 

Schuler, W.B. 3:134 

Schwam, F.R. 1:241 

Scott-honck, J.A. 5:29 

Seltzer, S.H. 3:111 

Sforzini , R.H. 3: 102 

Shapiro, A.H. 3:3 

Shaw, R. 1:84, 1:93, 1:129, 1:143 

Shawhan, S.O. 3:203 

Shaerer, R.E. 4:4 

Sheets, R.E. 2:97, 2:105 

Shephard, C.E. 2:77, 2:93 

Sherman, M.P. 2:111, 3:33 

Sherwood, P.J. 1:150, 1:164, 1:172, 

Shibata, Y. 2:146 

Shisetani, A. 2:142 

Shik, K.T. 2:104, 2:122 

Shiver, W.D. 2:118 

Shoji, 3.M. 3:164, 8:3 

Short, G.R. 3:41 

Short, R.A. 1:28, 1:40, 1:47, 1:58, 

3: 184 

3:54 

1:233, 1:236, 2:133 

3: 197 

1:215, 3:95 

Sanerville, J.M. 2:14 

Sopetto, L. 2:134 

Soquet, J. 3:96 

Sovey, J.S. 1:54, 1:67, 1:240 

Sovie, R.J. 3:85, 3:89, 3:97 

Spicer, L.M. 3:188, 3:192 

Spisz, E.W. 1:07, 1:14, 1:29, 2:48, 

Spongberg, R.M. 2:28 

Stark, K.W. 3:119 

Steenborg, M. 1:229, 1:236 

Stelts, P.D. 4:2 

Steward, R.B. 2:128 

Stephenson, W.B. 3:58 

Stine, H.A. 2:49, 2:93 

Stockbridge, C.D. 3: 137 

Stoner, W.A. 1:232, 2:17, 2:29, 2:39 

Stott, D. 1:185, 1:197 

Stratton, T.F. 3:132 

Stuhlinger, E. 1:115, 1:207, 3:109 

Suddeth, D.H. 3:136 

Surugue, J. 1:38 

Sutherland, G.S. 3:69 

Sutton, G.P. 3:5, 3:50 

Svedberg, R.C. 3:189 

Svehla, R.A. 3:40 

Szpankowski, R.J. 4: 16 

3:49 

2:58, 3:69 

Tmra, K. 5:19 

Tarifa, C.S. 3:120 

Tateho, H. 2:79 

Taylor, C.B. 1:229 

Tegart, J.R. 4:14 

Thieck, J. 1:83, 3:86, 3:107 

Thoenes, J. 9:18 

Tidnan, D.A. 6:l-4 

Tiedtke, P. 1:233 

Tinling, B.E. 3:41 

Tobias, I.J. 1:45, 2:96 

Todd, J.P. 

2: 105 

Traub, E. 2:2 

1:88, 2:50, 2:95, 2:97 

1:69, 1:70, 1:80, 1:81. 1:91, 1:106, Treat, R.P. 2:109 

1:112, 1:118, 1:140, 1:158. 1:159, Tuchan, A. 1:21 

3: 131 

Sievers, R.W. 3:136 

Silver, A.H. 1:46 

Sinpkins, P.S. 2:56 

Simons, G.A. 9:lO 

Singleton, A.H. 4:2 

Sinnette, J.T., Jr. 3:69 

Skifsted, J.G., 2:47, 2:94 

Smetana, F.O. 3:48 

Smith, N.S. 2:126 

Smith, W.W. 3:194, 3:202, 3:204 

Snyder, A. 3:135 

Turner, W.C. 3:126 

Twardy, H. 1:205, 3:165, 3:167, 3:173 

Uney, P. 4:12 

Urbach, H.B. 5:10, 5:13, 5:16 

Urrutie, J.L. 3:120 

Valentian, D. 3:107 

Valentini, R. 1:219, 3:174, 

Van Canp, W.M. 

VanLandinsham, E.€. 1:116, 1:117 

Vassalo, F.A. 3:22, 3:80 

Vaughn, G.F. 2:24 

2:98, 2:113, 3:186 

44 
Vinventi, R. 1:20, 1:30, 1:31 

Von Engel, A., 2:8 

Von Jaskwsky, W.F. 2:135 

Vondra, R.J. 1:230 

Walberg, G.D. 9:22 

Walker, J. 3:150 

Wallner, L.E. 2:106 

Walton, R. 3:87 

Wapato, P.G. 4:5 

Warner, 3:137 

Watakabe, Y. 2:142 

Watson, V.R. 

Weber, H.E. 2:109 

Weddelins, F. 5:5 

Weigand, A. 3:150 

Weinberg, A.F. 3:52 

2:49, 2:78, 2:93, 2:115 

Weiss, R.F. 9:2 

Weimn, J.I. 5:28 

Wells, R.C. 1:31 

Wells, W. 2:133 

Westbrook, J.H. 3:178 

White, A.F. 1:60 

White, R.E. 3:144 

Whitehair, S. 7:14, 7:15 

Widawsky, A. 3:42 

Wienecke, Z. 3:16, 3:17 

Wilkinson, H.C. 

Williw, J.C. 3:98 

Wiliiams, L.O. 3:156 

Williams, R.R. 3:138 

Williams, T. 3:119 

Willis, S.F. 1:116, 1:117 

1: 155, 4: 10 

Winsor, N.K. 6:1, 6:2, 6:3, 6:4 

Woidneck, H. 1:171, 3:133 

Wojnarwski, J. 3:184 

Wood, R.E. 3:183 

Wu, P.K.S. 9:5, 9:9 

Wutzke, S.A. 2:46, 2:90, 2:104, 2:116 

Yakut, H.H. 1:103 

Yarymovych, M. 2:51 

Yos, J.H. 2:52, 2:63, 2:130 

Yoshida, R.Y. 1:104-106, 1:118, 

1:119, 1:134, 1:136, 1:144 

Zafran, 5. 1:212, 1:237, 1:238 

Zaima, S. 2:146 

Zeimer, R.W. 3:23 

45 
1. Report No. 

NASA TM-86998 

A Bibliography of Electrothermal Thruster Technology, 

1984 

2. Government Accession No. 

7. Author(s) 

19. Security Classif. (of this report) 20. Security Classif. (of this page) 21. No. of pages 

Unclassified Uncl ass i f i ed 48 

James S. Sovey, Terry L. Hardy, and Matthew Englehart 

22. Price 

A03 

9. Performing Organization Name and Address 

National Aeronautics and Space Admlnistration 

Lewis Research Center 

Cleveland, Ohio 44135 

2. Sponsoring Agency Name and Address 

National Aeronautics and Space Administration 

Washington, D.C. 20546 

5. Supplementary Notes 

3. Recipient’s Catalog No. 

5. Report Date 

March 1986 

6. Performing Organization Code 

506-55-24 

I 8. Performing Organization Report No. 

E-2536 

10. Work Unit No. 

11. Contract or Grant No. 

13. Type of Report and Period Covered 

Technical Memorandum 

14. 

I 

Sponsoring Agency Code 

James S. Sovey and Terry L. Hardy, NASA Lewis Research Center; Matthew Englehart, 

Paper Basics, Brookpark, Ohio. 

6. Abstract 

Electrothermal propulsion concepts are briefly discussed as an introduction to a 

bibliography and author tndex for resistojets, thermal arcjets, pulsed electrothermal thrusters, microwave heated devices, solar thermal thrusters, and laser 

thermal thrusters. 

17. Key Words (Suggested by Author@)) 18. Distribution Statement 

Electrothermal thrusters; Arc jet; 

Resistojet; Auxiliary propulsion; 

Electric propulsion 

Unclassified - unlimited 

STAR Category 20