Publikationsdatum:
2019-07-13
Beschreibung:
The development and characteristics of advanced spacecraft fuel cell systems are discussed. The system is designed to operate on low pressure, propulsion grade hydrogen and oxygen. The specific goals are 10,000 hours of operation with refurbishment, 20 pounds per kilowatt at a sustained power of 7 KW, and 21 KW peaking capability for durations of two hours. The system rejects waste heat to the spacecraft cooling system at power levels up to 7 KW. At higher powers, the system automatically transfers to open cycle operation with overboard steam venting.
Schlagwort(e):
AUXILIARY SYSTEMS
Materialart:
NASA-TM-X-68033
,
E-6853
,
Power Sources Symp.; May 23, 1972 - May 25, 1972; Atlantic City
Format:
application/pdf
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