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Thermal control of a Mars entry capsule.Thermal control of Mars entry capsule with fiberglass honeycomb sandwich shell analyzed with and without aft thermal curtain, emphasizing cruise-flight phase
Document ID
19690057960
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Stultz, J. W.
Date Acquired
August 5, 2013
Publication Date
May 1, 1969
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 68-1082
Report Number: AIAA PAPER 68-1082
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
69A35949
Distribution Limits
Public
Copyright
Other

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