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
19680063991
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stultz, J. W.
Date Acquired
August 4, 2013
Publication Date
October 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 68-1082Report Number: AIAA PAPER 68-1082
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