The equipment, exclusive of thrustors, required to demonstrate the feasibility of a resistojet propulsion system for space station attitude control application using representative simulated crew biowaste propellants and available resistojet thrustors in the ground simulation tests is discussed. The overall objective of the program was to provide a biowaste resistojet prototype propellant management and control system sufficiently similar to the flight article to permit concept feasibility and system demonstration testing of interface compatibility, operational characteristics, and system flexibility. (Author)
Development of a Biowaste Resistojet Propulsion System
1973
122 pages
Report
Keine Angabe
Englisch
Development of a biowaste resistojet
NTRS | 1971
|Development of a biowaste resistojet
AIAA | 1971
|Development of a biowaste resistojet
AIAA | 1970
|