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ADVANCED VALVE TECHNOLOGY FOR SPACECRAFT ENGINES FINAL REPORTThis final report describes the work that was done to determine the state-of-the-art of valves required for space exploration vehicles and the steps that were taken to advance the technology. Interviews were held with personnel of major prime manufacturers to determine current problems and current and future requirements. Manufacturers were surveyed by mail to determine what equipment is presently being produced. An extensive search of patent office files was made to determine if any novel valve concepts not already applied to aerospace valves might exist. A literature search was conducted to provide the necessary technical information that was required for the program. Several extensive studies were made to determine the effects on materials resulting from use in space applications, and an investigation of the basic phenomena of valve seat wear was initiated. With the information developed in the surveys and studies, the significant problems associated with valves were identified and are described under "Discussion of Problems. " A novel valve concept was developed and a prototype valve was built and successfully tested. A seal compound of Teflon and stainless steel was developed which possesses superior cold flow characteristics while retaining the desirable properties of the basic Teflon material.
Document ID
19630005156
Acquisition Source
Jet Propulsion Laboratory
Document Type
Contractor or Grantee Report
Authors
B P Brady
(Space Technology Laboratories Redondo Beach, CA, United States)
R J Salvinski
(Space Technology Laboratories Redondo Beach, CA, United States)
Date Acquired
August 1, 2013
Publication Date
March 1, 1963
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
8651-6016-RU-000
Accession Number
63N15032
Funding Number(s)
CONTRACT_GRANT: NAS7-107
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Spacecraft propulsion
Spacecraft component
Valve
Rocket engine
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