Effect of Fuel and Design Options on RTG Performance versus PFF Power Demand
Paper presented at the 29th IECEC in Monterey, CA in August 1994. The present paper confines its attention to the relatively conservative option employing standard thermoelectric unicouples, since that may be the only one flight-ready for the projected PFF launch in 2001. There are four copies in the file; also a copy in the ESD files. Included in the file are two previous documents with the same title dated 4/18/1994.
- Research Organization:
- Fairchild Space and Defense Corporation
- Sponsoring Organization:
- NE Office of Space and Defense Power Systems
- OSTI ID:
- 1033364
- Report Number(s):
- AIAA-94-4128-CP; FSC-ESD-94-530; Orbital ID: 8575; Call Number: 34-05
- Country of Publication:
- United States
- Language:
- English
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