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Entry, Descent, and Landing Aerothermodynamics: NASA Langley Experimental Capabilities and ContributionsA review is presented of recent research, development, testing and evaluation activities related to entry, descent and landing that have been conducted at the NASA Langley Research Center. An overview of the test facilities, model development and fabrication capabilities, and instrumentation and measurement techniques employed in this work is provided. Contributions to hypersonic/supersonic flight and planetary exploration programs are detailed, as are fundamental research and development activities.
Document ID
20140007358
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hollis, Brian R. (NASA Langley Research Center Hampton, VA, United States)
Berger, Karen T. (NASA Langley Research Center Hampton, VA, United States)
Berry, Scott A. (NASA Langley Research Center Hampton, VA, United States)
Bruckmann, Gregory J. (NASA Langley Research Center Hampton, VA, United States)
Buck, Gregory M. (NASA Langley Research Center Hampton, VA, United States)
DiFulvio, Michael (NASA Langley Research Center Hampton, VA, United States)
Horvath, Thomas J. (NASA Langley Research Center Hampton, VA, United States)
Liechty, Derek S. (NASA Langley Research Center Hampton, VA, United States)
Merski, N. Ronald (NASA Langley Research Center Hampton, VA, United States)
Murphy, Kelly J. (NASA Langley Research Center Hampton, VA, United States)
Rufer, Shann J. (NASA Langley Research Center Hampton, VA, United States)
Schoenenberger, Mark (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 12, 2014
Publication Date
January 13, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-16744
AIAA Paper-2014-1154
Report Number: NF1676L-16744
Report Number: AIAA Paper-2014-1154
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting
Location: National Harbor, MD
Country: United States
Start Date: January 13, 2014
End Date: January 17, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 470883.04.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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