Application of parameter optimization techniques to space shuttle thermal protection designSpace shuttle thermal protection system optimal weight by numerical parameterization, discussing temperature constraints and material rearrangement effects
Document ID
19710045532
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Curry, D. M.
Williams, S. D.
Date Acquired
August 6, 2013
Publication Date
April 1, 1971
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,