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Space transportation booster engine thrust chamber technology, large scale injectorThe objective of the Large Scale Injector (LSI) program was to deliver a 21 inch diameter, 600,000 lbf thrust class injector to NASA/MSFC for hot fire testing. The hot fire test program would demonstrate the feasibility and integrity of the full scale injector, including combustion stability, chamber wall compatibility (thermal management), and injector performance. The 21 inch diameter injector was delivered in September of 1991.
Document ID
19930017368
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schneider, J. A.
(GenCorp Aerojet Sacramento, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-192531
NAS 1.26:192531
Report Number: NASA-CR-192531
Report Number: NAS 1.26:192531
Accession Number
93N26557
Funding Number(s)
CONTRACT_GRANT: NAS8-37470
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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