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Thermal Protection System (Heat Shield) Development - Advanced Development ProjectThe Orion Thermal Protection System (TPS) ADP was a 3 1/2 year effort to develop ablative TPS materials for the Orion crew capsule. The ADP was motivated by the lack of available ablative TPS's. The TPS ADP pursued a competitive phased development strategy with succeeding rounds of development, testing and down selections. The Project raised the technology readiness level (TRL) of 8 different TPS materials from 5 different commercial vendors, eventual down selecting to a single material system for the Orion heat shield. In addition to providing a heat shield material and design for Orion on time and on budget, the Project accomplished the following: 1) Re-invigorated TPS industry & re-established a NASA competency to respond to future TPS needs; 2) Identified a potentially catastrophic problem with the planned MSL heat shield, and provided a viable, high TRL alternate heat shield design option; and 3) Transferred mature heat shield material and design options to the commercial space industry, including TPS technology information for the SpaceX Dragon capsule.
Document ID
20100036525
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Kowal, T. John
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
October 13, 2010
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-21831
Report Number: JSC-CN-21831
Meeting Information
Meeting: Commercial Human Spaceflight Symposium
Location: Houston, TX
Country: United States
Start Date: October 13, 2010
End Date: October 14, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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