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Apollo entry aerodynamics.Apollo spacecraft command module aerodynamic characteristics during entry compared with wind tunnel test predictions
Document ID
19690048800
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Crowder, R. S.
Moote, J. D.
Date Acquired
August 5, 2013
Publication Date
March 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 68-1008
Report Number: AIAA PAPER 68-1008
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ANNUAL MEETING AND TECHNICAL DISPLAY
Location: PHILADELPHIA, PA
Start Date: October 21, 1968
End Date: October 24, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A26789
Funding Number(s)
CONTRACT_GRANT: NAS9-150
Distribution Limits
Public
Copyright
Other

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