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Potential propellant storage and feed systems for space station resistojet propulsion options. Final report

Technical Report ·
OSTI ID:6728875
The resistojet system has been defined as part of the baseline propulsion system for the initial Operating Capability Space Station. The resistojet propulsion module will perform a reboost function using a wide variety of fluids as propellants. There are many optional propellants and propellant combinations for use in the resistojet including (but not limited to): hydrazine, hydrogen, oxygen, nitrogen, water, carbon dioxide, and methane. Many different types of propulsion systems have flown or have been conceptualized that may have application for use with resistojets. This paper describes and compares representative examples of these systems that may provide a basis for space station resistojet system design.
Research Organization:
Sverdrup Technology, Inc., Cleveland, OH (USA)
OSTI ID:
6728875
Report Number(s):
N-87-16065; NASA-CR-179457; E-3366; NAS-1.26:179457
Country of Publication:
United States
Language:
English