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Apollo entry aerodynamics.
Apollo spacecraft command module aerodynamic characteristics during entry compared with wind tunnel test predictions
Document ID
19680063975
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Crowder, R. S.
Moote, J. D.
Date Acquired
August 4, 2013
Publication Date
October 1, 1968
Publication Information
Publisher:
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 68-1008
Report Number: AIAA PAPER 68-1008
Meeting Information
Meeting:
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
68A44947
Funding Number(s)
CONTRACT_GRANT: NAS9-150
Distribution Limits
Public
Copyright
Other
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