NASA NTRS · 19960021862
Computed Flow About The Integrated Space Shuttle, Revisited
Abstract
Report 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.
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Buning, P. G., Obayashi, S., Steger, J. L., Chiu, I. T., Martin, F. W., Jr., Meakin, R. L., Rizk, Y. M., Yarrow, M.. 1996-04-01. Computed Flow About The Integrated Space Shuttle, Revisited. https://ntrs.nasa.gov/citations/19960021862
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