NASA NTRS · 19740018866
Liquid rocket valve assemblies
Abstract
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.
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1973-11-01. Liquid rocket valve assemblies. https://ntrs.nasa.gov/citations/19740018866
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