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NASA/SP-8119, NASA SPACE VEHICLE DESIGN CRITERIA (CHEMICAL PROPULSION): LIQUID ROCKET DISCONNECTS, COUPLINGS, FITTINGS, FIXED JOINTS, AND SEALS (SEP-1976)

NASA/SP-8119, NASA SPACE VEHICLE DESIGN CRITERIA (CHEMICAL PROPULSION): LIQUID ROCKET DISCONNECTS, COUPLINGS, FITTINGS, FIXED JOINTS, AND SEALS (SEP-1976)., State of the art and design criteria for components used in liquid propellant rocket propulsion systems to contain and control the flow of fluids involved are discussed. Particular emphasis is placed on the design of components used in the engine systems of boosters and upper stages, and in spacecraft propulsion systems because of the high pressure and high vibration levels to which these components are exposed. A table for conversion of U.S. customary units to SI units is included with a glossary, and a list of NASA space vehicle design criteria monographs issued to September 1976.

SP-8119 Rev. 1976

    
 Status:
Inactive

 FSC Code:
 1810 - Space Vehicles

Version:
197608-19767.35 MB NASA_SP-8119_SEP1976

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