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A parametric analysis of three vehicle shapes for use as hyperbolic entry.Apollo command module, biconic and cone hyperbolic reentry vehicles engineering, discussing L/D ratio, heat protection and weight
Document ID
19680036593
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, J. L.
Swenson, B. L.
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 68-152
Report Number: AIAA PAPER 68-152
Meeting Information
Meeting: AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 22, 1968
End Date: January 24, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A17565
Distribution Limits
Public
Copyright
Other

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