NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Cast segment evaluationEvaluation program to determine feasibility of fabricating segmented rocket engine thrust chambers using low cost, lightweight castings extends state of the art in areas of casting size and complexity, and in ability to provide thin sections and narrow, deep, cooling channels. Related developments are discussed.
Document ID
19710000361
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Diem, H. G.
(ROCKETDYNE)
Studhalter, W. R.
Date Acquired
August 6, 2013
Publication Date
September 1, 1971
Subject Category
Fabrication Technology
Report/Patent Number
MFS-21354
Report Number: MFS-21354
Accession Number
71B10363
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available