Liquid rocket valve assemblies, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8097, Liquid rocket valve assemblies, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), November,1973, pp. 154, Format(s): PDF 8985k

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The design and operating characteristics of valve assemblies used in liquid propellant rocket engines are discussed. The subjects considered are as follows: (1) valve selection parameters, (2)major design aspects, (3) design integration of valve subassemblies, and (4) assembly of components and functional tests. Information is provided on engine, stage, and spacecraft checkout procedures.

Keywords:	machine elements and processes, butterfly valves, control valves, fuel valves, liquid propellant rocket engines, equipment specifications, hydraulic equipment, structural design criteria
CASI Document ID Number:	74N26979
Subjects:	Astronautics: Spacecraft Propulsion And Power: Rocket Engines, Nozzles And Thrust Chambers
ID Code:	149
Deposited On:	23 May 2002