Results of first phase of program to define resistojet control system for manned orbiting research laboratory (MORL); 10-mib hydrogen ammonia, and biowaste thruster systems are defined to satisfy impulse requirements arising from aerodynamic and gravity-gradient forces in orbit; of available biowastes (H2, Co2 and fecal water), CO2 output alone was sufficient to provide impulse requirements for 10-mlb system; however, combined CO2/H2 system permits greater growth capability at expense of simplicity; use of resistojet thruster system to provide orbit injection and high-disturbance control impulse was also investigated.
Subsystems analyses for MORL resistojet control system
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 5 , n 8
1968
7 pages
Article (Journal)
English
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Subsystem analyses for a MORL resistojet control system
AIAA | 1967
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|Morl Control System Integration
NTIS | 1964
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