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An Innovative Solution to NASA's NEO Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture DevelopmentTo develop an innovative yet practically implementable mitigation technique for the most probable impact threat of an asteroid or comet with short warning time(i.e., when we don't have sufficient warning times for a deflection mission)
Document ID
20150022453
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Wie, Bong (Iowa State Univ. Ames, IA, United States)
Barbee, Brent (NASA Goddard Space Flight Center Greenbelt, MD United States)
Pitz, Alan (Iowa State Univ. Ames, IA, United States)
Kaplinger, Brian (Iowa State Univ. Ames, IA, United States)
Hawkins, Matt (Iowa State Univ. Ames, IA, United States)
Winkler, Tim (Iowa State Univ. Ames, IA, United States)
Premaratne, Pavithra (Iowa State Univ. Ames, IA, United States)
Vardaxis, George (Iowa State Univ. Ames, IA, United States)
Lyzhoft, Joshua (Iowa State Univ. Ames, IA, United States)
Zimmerman, Ben (Iowa State Univ. Ames, IA, United States)
Date Acquired
December 8, 2015
Publication Date
April 16, 2015
Subject Category
Astrodynamics
Report/Patent Number
GSFC-E-DAA-TN22340
Meeting Information
Meeting: IAA Planetary Defense Conference
Location: Frascati
Country: Italy
Start Date: April 13, 2015
End Date: April 17, 2015
Sponsors: International Academy of Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
NEO Impact threat
Planetary defense
Mitigation

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