Development of a hydrogen-oxygen internal combustion engine space power system |
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AISI ambient BMEP brazed BSPC calcium fluoride cam follower chrome plate clearance volume combustion chamber configuration coolant cooling crankcase cylinder head insert cylinder head ring cylinder pressure Data Sheet endurance test evaluation exhaust pressure Flame plated flex pivot friction gasket H2 Valve hardware Haynes 25 heat rejection heated hydrogen high pressure ratios horsepower hydrogen inlet hydrogen valve Inconel increased inlet pressure inlet temperature inlet valve input internal combustion engine leak leakage mass flow rate NASA NASA CONTRACT O/F ratio Oj Injector operating outer valve oxygen injector pellets performance test piston dome Piston Pin poppet poppet valve PROTOTYPE COMPRESSOR psig quill shaft reduce Retainer ring belt rocker arm rocker shaft Rulon seal installed seat second stage shown in Figure speed Stainless Stellite teflon Temp test stand tool steel torque v/CF valve assembly valve spring volumetric efficiency wear rate
Bibliographic information
| Title | Development of a hydrogen-oxygen internal combustion engine space power system NASA contractor report |
| Author | W. D. Morath |
| Publisher | National Aeronautics and Space Administration, 1965 |
| Original from | National Aeronautics and Space Administration (NASA) |
| Digitized | Feb 4, 2010 |
| Length | 204 pages |
| Export Citation | BiBTeX EndNote RefMan |