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On the Development of a New Nonequilibrium Chemistry Model for Mars EntryThis paper represents an on-going effort at NASA Ames Research Center to develop a physics-based nonequilibrium model for hypersonic entry into the Martian atmosphere.
Document ID
20170000840
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Jaffe, R. L. (NASA Ames Research Center Moffett Field, CA United States)
Schwenke, D. W. (NASA Ames Research Center Moffett Field, CA United States)
Chaban, G. M. (NASA Ames Research Center Moffett Field, CA United States)
Prabhu, D. K. (NASA Ames Research Center Moffett Field, CA United States)
Johnston, C. O. (NASA Langley Research Center Hampton, VA, United States)
Panesi, M. (Illinois Univ. Urbana-Champaign, IL, United States)
Date Acquired
January 26, 2017
Publication Date
January 11, 2017
Subject Category
Atomic And Molecular Physics
Inorganic, Organic And Physical Chemistry
Astronautics (General)
Report/Patent Number
ARC-E-DAA-TN38595
Meeting Information
Meeting: AIAA SciTech 2017
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA15BB15CB
WBS: WBS 470883.04.01.0
CONTRACT_GRANT: NNX15AU44G
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
potetnial energy surface
nonequilibrium
quasiclassical trajectory calculation

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