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Sharp Technologies as Applied to a Crew Transfer Vehicle (CTV)This viewgraph presentation reviews the efforts of Ames Research Center to develop Slender Hypersonic Aerothermodynamic Research Probes (SHARP) technologies as applied to the new Crew Transfer Vehicle (CTV). Amongst these technologies are ultra high temperature ceramics (UHTC). The results of Computational Fluid Dynamic simulations on prospective designs of the CTV are shown as well as wind tunnel test results.
Document ID
20060050750
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Cappuccio, Gelsomina (NASA Ames Research Center Moffett Field, CA, United States)
Kinney, David (NASA Ames Research Center Moffett Field, CA, United States)
Reuther, James (NASA Ames Research Center Moffett Field, CA, United States)
Saunders, David (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Spacecraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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