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An Innovative Solution to NASA's NEO Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture DevelopmentThis final technical report describes the results of a NASA Innovative Advanced Concept (NIAC) Phase 2 study entitled "An Innovative Solution to NASA's NEO Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture Development." This NIAC Phase 2 study was conducted at the Asteroid Deflection Research Center (ADRC) of Iowa State University in 2012-2014. The study objective was to develop an innovative yet practically implementable solution to the most probable impact threat of an asteroid or comet with short warning time (less than 5 years). The technical materials contained in this final report are based on numerous technical papers, which have been previously published by the project team of the NIAC Phase 1 and 2 studies during the past three years. Those technical papers as well as a NIAC Phase 2 Executive Summary report can be downloaded from the ADRC website (www.adrc.iastate.edu).
Document ID
20190001168
Acquisition Source
Headquarters
Document Type
Contractor or Grantee Report
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)
Wagner, Sam
(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
March 4, 2019
Publication Date
December 9, 2014
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
HQ-E-DAA-TN63107
Report Number: HQ-E-DAA-TN63107
Funding Number(s)
CONTRACT_GRANT: NNX12AQ60G
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
NEO
Research
Comet
Asteroid
Impact Threat
Deflection
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