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Computed Flow About The Integrated Space Shuttle, RevisitedReport discusses numerical simulations of flow of air about integrated space shuttle (complete space shuttle assembly including orbiter, solid rocket boosters, and external tank) in ascent. Updated version of report described in "Computed Flow About The Integrated Space Shuttle" (ARC-12685). Goal of studies to improve understanding of, and ability to predict how integrated space shuttle performs during both nominal and aborted ascent under various conditions.
Document ID
19960021862
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Buning, P. G. (NASA Ames Research Center, Moffett Field, CA.)
Obayashi, S. (NASA Ames Research Center, Moffett Field, CA.)
Steger, J. L. (NASA Ames Research Center, Moffett Field, CA.)
Chiu, I. T. (Iowa State Univ.)
Martin, F. W., Jr. (Johnson Space Center)
Meakin, R. L. (Sterling Software)
Rizk, Y. M. (Sterling Software)
Yarrow, M. (Sterling Software)
Date Acquired
August 17, 2013
Publication Date
April 1, 1996
Publication Information
Publication: NASA Tech Briefs
Volume: 20
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-13163
Accession Number
96B10198
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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