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Fabrication of liquid-rocket thrust chambers by electroformingElectroforming has proven to be an excellent fabrication method for building liquid rocket regeneratively cooled thrust chambers. NASA sponsored technology programs have investigated both common and advanced methods. Using common procedures, several cooled spool pieces and thrust chambers have been made and successfully tested. The designs were made possible through the versatility of the electroforming procedure, which is not limited to simple geometric shapes. An advanced method of electroforming was used to produce a wire-wrapped, composite, pressure-loaded electroformed structure, which greatly increased the strength of the structure while still retaining the advantages of electroforming.
Document ID
19750002100
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Duscha, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Kazaroff, J. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1974
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-7987
NASA-TM-X-3116
Report Number: E-7987
Report Number: NASA-TM-X-3116
Accession Number
75N10172
Funding Number(s)
PROJECT: RTOP 502-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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