Power Systems for Space Flight 1963
DOI: 10.1016/b978-0-12-395680-4.50016-2
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Development of Catalytic Hydrogen-Oxygen Reaction Chambers for Space Power Systems

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1966
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“…9 is 34.3% at the generator terminals, with a compressor inlet temperature of 50°F. The weight of the complete system is estimated at 2500 Ib, less shielding and pressure vessel, and volume at 35 ft 3 . Sea water can be utilized for a portion of the shielding.…”
Section: Long-duration Mission With Liquid-metal-cooled Nuclear mentioning
confidence: 99%
“…9 is 34.3% at the generator terminals, with a compressor inlet temperature of 50°F. The weight of the complete system is estimated at 2500 Ib, less shielding and pressure vessel, and volume at 35 ft 3 . Sea water can be utilized for a portion of the shielding.…”
Section: Long-duration Mission With Liquid-metal-cooled Nuclear mentioning
confidence: 99%