NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Thermal Protection System of the Space ShuttleThe Thermal Protection System (TPS), introduced by NASA, continues to incorporate many of the advances in materials over the past two decades. A comprehensive, single-volume summary of the TPS, including system design rationales, key design features, and broad descriptions of the subsystems of TPS (E.g., reusable surface insulation, leading edge structural, and penetration subsystems) is provided. Details of all elements of TPS development and application are covered (materials properties, manufacturing, modeling, testing, installation, and inspection). Disclosures and inventions are listed and potential commercial application of TPS-related technology is discussed.
Document ID
19890016675
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cleland, John
(Research Triangle Inst. Research Triangle Park, NC., United States)
Iannetti, Francesco
(Design Ideas Raleigh, NC., United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1989
Subject Category
Chemistry And Materials (General)
Report/Patent Number
NASA-CR-4227
NAS 1.26:4227
Report Number: NASA-CR-4227
Report Number: NAS 1.26:4227
Accession Number
89N26046
Funding Number(s)
CONTRACT_GRANT: NASW-3841
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available