Development of a Hydrogen-oxygen Internal Combustion Engine Space Power SystemClearinghouse for Federal Scientific and Technical Information, 1965 - Internal combustion engines - 200 pages |
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Common terms and phrases
AISI allow ambient assembly bearing BSPC clearance combustion chamber compressor configuration Contract cooling cylinder head discharge dome drive linkage effect efficiency effort endurance test energy engine evaluation exhaust Failure final flow follower friction hardware Haynes heat higher hydrogen valve improvement inch increased indicates inlet inlet pressure inlet temperature input insert installed internal leak leakage less levels limited load loss lower lubrication material measured NASA O/F ratio operating oxygen injector pellets performance piston Piston Pin pivot plated poppet possible present pressure ratio problems prototype psig reduce Retainer ring rocker arm Rulon seal seat second stage shaft Sheet shown in Figure shows speed spring stage steel supply surface Table taken teflon temperature test stand values valve spring volume wear weight
Bibliographic information
| Title | Development of a Hydrogen-oxygen Internal Combustion Engine Space Power System NASA contractor report, United States National Aeronautics and Space Administration |
| Authors | Norman Evan Morgan, W. D. Morath |
| Contributors | Vickers, Incorporated, United States. National Aeronautics and Space Administration |
| Publisher | Clearinghouse for Federal Scientific and Technical Information, 1965 |
| Original from | National Aeronautics and Space Administration (NASA) |
| Digitized | Feb 4, 2010 |
| Length | 200 pages |
| Export Citation | BiBTeX EndNote RefMan |