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Rocket Engine Thrust Chamber AssemblyA thrust chamber assembly for liquid fueled rocket engines and the method of making it wherein a two-piece mandrel wrapped with a silica tape saturated with a phenolic resin, the tape extending along the mandrel and covering the combustion chamber portion of the mandrel to the throat portion. The phenolic in the tape is cured and the end of the wrap is machined. The remainder of the mandrel is wrapped with a third silica tape. The resin in the third tape is cured and the assembly is machined. The entire assembly is then wrapped with a tow of graphite fibers wetted with an epoxy resin and, after the epoxy resin is cured, the graphite is machined to final dimensions.
Document ID
20020034153
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
Authors
Cornelius, Charles S.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Counts, Richard H.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Myers, W. Neill
(NASA Marshall Space Flight Center Huntsville, AL United States)
Lackey, Jeffrey D.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Peters, Warren
(NASA Marshall Space Flight Center Huntsville, AL United States)
Shadoan, Michael D.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Sparks, David L.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Lawrence, Timothy W.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 20, 2013
Publication Date
December 18, 2001
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
Patent Number: NASA-Case-MFS-31138-2-Div
Patent Number: US-Patent-6,330,792
Patent Application Number: US-Patent-Appl-SN-228034
Patent Application Number: US-Patent-Appl-SN-747979
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-MFS-31138-2-Div|US-Patent-6,330,792
Patent Application
US-Patent-Appl-SN-228034|US-Patent-Appl-SN-747979
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