The thermoelectric outer-planet spacecraft (TOPS) attitude propulsion subsystem effort is summarized. It includes the tradeoff rationale that went into the selection of anhydrous hydrazine as the propellant, and a brief description of three types of 0.445-N (100-mlbf) thrusters that were purchased for in-house evaluation. A discussion is also included of the 0.2224-N (50-mlbf)-developed thrusters and their integration with a portable, completely enclosed, propulsion module that was designed and developed to support the TOPS single-axis attitude control tests in the celestarium.
TOPS attitude propulsion subsystem technology
1971-10-01
Miscellaneous
No indication
English
TOPS spacecraft propulsion subsystem
NTRS | 1970
|Attitude propulsion technology for TOPS
NTRS | 1972
|Attitude Propulsion Technology for Tops
NTIS | 1972
|Spacecraft radio - TOPS radio frequency subsystem
NTRS | 1970
|NTRS | 1970
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