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Space shuttle: Effect of orbiter incidence angle on the aerodynamic characteristics of the Boeing S-IC booster/ GAC G-11 orbiter launch configuration, M equal .6 to 4.96Wind tunnel stability tests of space shuttle model at subsonic to hypersonic speeds
Document ID
19710029199
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Watts, L. L. (Chrysler Corp. New Orleans, LA, United States)
Date Acquired
August 6, 2013
Publication Date
August 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
DMS-DR-1140
NASA-CR-119981
Accession Number
71N38675
Funding Number(s)
CONTRACT_GRANT: NAS8-4016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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