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Space Shuttle Orbiter - Reusable surface insulation flight performanceThe first two flights of the Space Shuttle Orbiter have provided the initial data required for operational certification of the Thermal Protection System (TPS). The flight performance characteristics of the TPS reusable surface insulation (RSI) will be discussed. The discussion will be based on post-flight inspections of the RSI and post-flight interpretations of the flight instrumentation data. The flights to date indicate that the thermal and mechanical design requirements for the RSI system were met or exceeded.
Document ID
19820046543
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Dotts, R. L.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Tillian, D. J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Smith, J. A.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 82-0788
Meeting Information
Meeting: In: Structures, Structural Dynamics and Materials Conference
Location: New Orleans, LA
Start Date: May 10, 1982
End Date: May 12, 1982
Accession Number
82A30078
Distribution Limits
Public
Copyright
Other

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