This paper discusses the engine system and component design of the J-2 liquid propellant rocket engine, with emphasis upon the newer features whose development has been dictated by the use of liquid hydrogen as the fuel. A brief description of the development program and of the principal specialized test equipment is given.
The J-2 Liquid Hydrogen Rocket Engine
Sae Technical Papers
SAE World Congress & Exhibition ; 1964
1964-01-01
Conference paper
English
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