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Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Technology Development OverviewThe successful flight of the Inflatable Reentry Vehicle Experiment (IRVE)-3 has further demonstrated the potential value of Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology. This technology development effort is funded by NASA's Space Technology Mission Directorate (STMD) Game Changing Development Program (GCDP). This paper provides an overview of a multi-year HIAD technology development effort, detailing the projects completed to date and the additional testing planned for the future.
Document ID
20130014935
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Hughes, Stephen J. (NASA Langley Research Center Hampton, VA, United States)
Cheatwood, F. McNeil (NASA Langley Research Center Hampton, VA, United States)
Calomino, Anthony M. (NASA Langley Research Center Hampton, VA, United States)
Wright, Henry S. (NASA Langley Research Center Hampton, VA, United States)
Wusk, Mary E. (NASA Langley Research Center Hampton, VA, United States)
Hughes, Monica F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
December 30, 2013
Publication Date
June 17, 2013
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-16795
Report Number: NF1676L-16795
Meeting Information
Meeting: International Planetary Probe Workshop (IPPW-10)
Location: San Jose, CA
Country: United States
Start Date: June 17, 2013
End Date: June 21, 2013
Sponsors: NASA Ames Research Center, San Jose State Univ.
Funding Number(s)
WBS: WBS 677714.04.01.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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