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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
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
IAA Planetary Defense Conference(Frascati)
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
NEO Impact threat
Planetary defense
Mitigation

Available Downloads

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