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Liquid rocket disconnects, couplings, fittings, fixed joints, and seals, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8119, Liquid rocket disconnects, couplings, fittings, fixed joints, and seals, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA (Washington, DC, United States), September,1976, pp. 164, Format(s): PDF 9638k

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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.
Keywords:spacecraft propulsion and power, couplings, disconnect devices, fittings, joints (junctions), liquid propellant rocket engines, seals, (stoppers), engine parts, equipment specifications, fluid transmission lines, fuel flow regulators, propulsion system configurations
CASI Document ID Number:77N24191
Subjects:Astronautics: Spacecraft Propulsion And Power
ID Code:185
Deposited On:06 June 2002