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STS-1 Nominal Cycle 3 March/April Launch, Ascent Base Convective Heating EnvironmentsAscent base convective heating environments were determined for the nominal ascent trajectory for the STS-1 Cycle 3 March/April launch period. Both first and second stage environments are defined for all base heating DFI locations and design body points of interest. An identical format to the STS-1 dispersed trajectory environment was followed throughout. As expected, STS-1 nominal environments are generally less severe than those determined for the high loft and low loft dispersed trajectory conditions. The reduction in cold wall heating with the nominal trajectory varies for each base location analyzed, but, in general, was approximately twenty percent.
Document ID
19810006500
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bender, R. L., Jr.
(Remtech, Inc. Huntsville, AL, United States)
Lee, Y. C.
(Remtech, Inc. Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
November 24, 1980
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-161629
Report Number: NASA-CR-161629
Accession Number
81N15015
Funding Number(s)
CONTRACT_GRANT: NAS8-33725
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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