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The NASA Sharp Flight ExperimentThe Slender Hypersonic Aerothermodynamic Research Program (SHARP) was initiated by NASA Ames, and executed in partnership with Sandia National Laboratory and the US Air Force, to demonstrate sharp, passive leading edge designs for hypersonic vehicles, incorporating new ultra-high temperature ceramics (UHTC's). These new ceramic composites have been undergoing development, characterization and ground testing at NASA Ames for the last nine years. This paper will describe the background, flight objectives, design and pertinent flight results of SHARP, and some of the potential implications for future hypersonic vehicle designs.
Document ID
20020051881
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Rasky, Daniel J.
(NASA Ames Research Center Moffett Field, CA United States)
Salute, Joan
(NASA Ames Research Center Moffett Field, CA United States)
Kolodziej, Paul
(NASA Ames Research Center Moffett Field, CA United States)
Bull, Jeffrey
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
August 20, 2013
Publication Date
January 1, 1998
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: 3rd European Workshop on Thermal Protection Systems
Location: Noordwijk
Country: Netherlands
Start Date: March 25, 1998
End Date: March 27, 1998
Sponsors: European Space Agency. European Space Research and Technology Center, ESTEC
Funding Number(s)
PROJECT: RTOP 242-72-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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