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Liquid rocket disconnects, couplings, fittings, fixed joints, and sealsState 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.
Document ID
19770017247
Document Type
Special Publication (SP)
Date Acquired
September 3, 2013
Publication Date
September 1, 1976
Subject Category
SPACECRAFT PROPULSION AND POWER
Report/Patent Number
NASA-SP-8119
Funding Number(s)
CONTRACT_GRANT: NAS3-12068
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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NameType 19770017247.pdf STI