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NLS cycle 1 and NLS 2 base heating technical notes. Appendix 3: Preliminary cycle 1 NLS base heating environments. Cycle 1 NLS base heating environments. NLS 2 650K STME base heating environmentsA preliminary analysis of National Launch System ascent plume induced base heating environments has been completed to support the Induced Environments Panel's objective to assist in maturing the NLS vehicle (1.5 stage and heavy launch lift vehicle) design. Environments during ascent have been determined from this analysis for a few selected locations on the engine nozzles and base heat shield for both vehicles. The environments reflect early summer 1991 configurations and performance data and conservative methodology. A more complete and thorough analysis is under way to update these environments for the cycle 1 review in January 1992.
Document ID
19930012823
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bender, Robert L.
(Remtech, Inc. Huntsville, AL, United States)
Reardon, John E.
(Remtech, Inc. Huntsville, AL, United States)
Prendergast, Maurice J.
(Remtech, Inc. Huntsville, AL, United States)
Schmitz, Craig P.
(Remtech, Inc. Huntsville, AL, United States)
Brown, John R.
(Remtech, Inc. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
RTN-218-03
RTN-218-04
RTN-218-01
RTN-250-6-01
NAS 1.26:192454
NASA-CR-192454
Report Number: RTN-218-03
Report Number: RTN-218-04
Report Number: RTN-218-01
Report Number: RTN-250-6-01
Report Number: NAS 1.26:192454
Report Number: NASA-CR-192454
Accession Number
93N22012
Funding Number(s)
CONTRACT_GRANT: NAS8-38141
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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