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The Space ShuttleThe development of the Space Shuttle is traced. Aerodynamic loads and dynamic characteristics, structural design, ascent and entry heating profiles, and propulsion systems are discussed. Problems in the area of systems management and flight control during entry and in the design of an effective thermal control system are discussed in detail.
Document ID
19810060230
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Faget, M. A. (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Space Transportation
Report/Patent Number
AAS 80-292
Meeting Information
Meeting: Annual Meeting Space - Enhancing technological leadership
Location: Boston, MA
Start Date: October 20, 1980
End Date: October 23, 1980
Accession Number
81A44634
Distribution Limits
Public
Copyright
Other

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