Report discusses numerical simulations of flow of air about integrated Space Shuttle in ascent. Goal: to improve understanding of, and ability to predict, how integrated Space Shuttle will perform during both nominal and aborted ascent under various conditions. These and other numerical simulations intended both to supplement wind-tunnel data, corrupted to some extent by scaling and wall-interference effects, and to compensate for scarcity of valid flight data.
Computed Flow About The Integrated Space Shuttle
NASA Tech Briefs ; 15 , 10
1991-10-01
Miscellaneous
No indication
English
Computed Flow About the Integrated Space Shuttle, Revisited
Online Contents | 1996
Integrated electronics system for space shuttle
AIAA | 1970
|Integrated electronics for the space shuttle
AIAA | 1970
|Integrated Electronics for the Space Shuttle
AIAA | 1971
|