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Current Technology for Thermal Protection SystemsInterest in thermal protection systems for high-speed vehicles is increasing because of the stringent requirements of such new projects as the Space Exploration Initiative, the National Aero-Space Plane, and the High-Speed Civil Transport, as well as the needs for improved capabilities in existing thermal protection systems in the Space Shuttle and in turbojet engines. This selection of 13 papers from NASA and industry summarizes the history and operational experience of thermal protection systems utilized in the national space program to date, and also covers recent development efforts in thermal insulation, refractory materials and coatings, actively cooled structures, and two-phase thermal control systems.
Document ID
19930003259
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Scotti, Stephen J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CP-3157
NAS 1.55:3157
L-17118
Accession Number
93N12447
Funding Number(s)
PROJECT: RTOP 506-43-31-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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