Space storable hydrocarbon fuel blended FLOX propellant performance with coaxial injector including characteristic velocity, chamber geometry, pressure and heat flux distribution
Space storable propellant performance with the coaxial injector.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE ; 1969 ; COLORADO SPRINGS, COLO.
1969-06-01
Conference paper
No indication
English
Coaxial Injector Development for Storable Propellant Upper Stage Turbopump Engines
British Library Conference Proceedings | 1997
|Space storable propellant performance demonstration
AIAA | 1969
|Space storable propellant performance demonstration.
NTRS | 1969
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