Large impulses of self-magnetic origin
Self magnetic impulses in gas discharge configuration as function of current and anode- cathode radii ratio
Garrison, R. L.↗
Engineering topics
John, R. R.
Publications and source records attributed to John, R. R..
Quasi-steady MPD propulsion at high power Final technical report
Quasi-steady MPD propulsion at power levels in range 1 to 10 megawatts
Garrison, R. L.↗
Outstanding problems regarding the feasibility of a repetitively pulsed MPD propulsion system
Repetitively pulsed MPD propulsion systems, considering thrustor performance
John, R. R.↗
High power quasi-steady MPD acceleration Final report
High power quasi-steady MPD acceleration
John, R. R.↗
Development of an ammonia-fueled MPD arc jet thruster.
Steady flow ammonia MPD arc jet thrustor propulsion performance, discussing test chamber pressure variation, thrust data and cooling systems
THRUSTOR↗
Design, development, fabrication, test and delivery of electrothermal engine systems Semiannual report, Dec. 1965 - Jun. 1966
Ammonia fueled resistojet thrustor system for three-axis attitude control and two-direction station-keeping of stable platform type satellite
PROPULSION SYSTEM↗
S-Band laboratory test equipment Final report
Subsystem component design and development, and system performance of ammonia fueled resistojet thrustor for spacecraft inversion maneuvers
RESISTOJET ENGINE↗
Recent advances in electrothermal and hybrid electrothermal-electromagnetic propulsion.
Performance and applications of electrothermal and hybrid electrothermal electromagnetic space propulsion
Bennett, S.↗
Cesium fueled mpd arc jet engine performance.
MPD arc thrustor operated with cesium plasma and external magnetic field
ARC JET↗
Recent advances in electrothermal and hybrid electrothermal-electromagnetic propulsion.
Performance and applications of electrothermal and hybrid electrothermal-electromagnetic space propulsion
ARC JET↗
Experimental performance of a high specific impulse arc jet engine.
Liquid cooled high specific impulse arc jet engine has measured engine thrust not completely aerodynamic in nature
ARC JET↗
Resistojet research and development, phase ii second quarterly progress report, 1 oct. - 31 dec. 1964
Transient propulsion performance of 10 watt fast heating resistojet engine
PROPULSION SYSTEM PERFORMANCE↗
Experimental propulsion performance of a low power pulsed resistojet.
Low power pulsed resistojet applied to orbit and attitude control and station keeping of 500-lb synchronous satellite
SATELLITE ATTITUDE CONTROL↗
Experimental propulsion performance of a low power pulsed resistojet.
Performance data of resistojet designed for attitude control and station keeping of 500-lb synchronous satellite
RESISTOJET ENGINE↗
Resistojet research and development - phase ii first quarterly progress report, 6 jul. - 30 sep. 1964
Pulsed and continuous resistojet thrustors for attitude control and station keeping of synchronous satellite
SATELLITE ATTITUDE CONTROL↗
Nuclear-electric power requirements for electric rockets
Nuclear-electric power requirements for electric rockets - contact and bombardment ion engines, arc jets, and pulsed plasma engines
ARC JET↗
ARCJET ENGINE PERFORMANCE- EXPERIMENT AND THEORY
Performance of a hydrogen radiation-cooled arc jet engine, with emphasis on power conversion efficiency and the energy addition and loss mechanism
POWER CONVERSION↗
THIRTY DAY ENDURANCE TEST OF A 30KW ARC JET ENGINE
Observations on the energy transfer processes occurring within the arc jet engine
ENERGY TRANSFER↗