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Options and Uncertainties in Planetary Defense: Mission Planning and Vehicle Design for Flexible ResponseThis paper is part of an integrated study by NASA and the NNSA to quantitatively understand the response timeframe should a threatening Earth-impacting near-Earth object (NEO) be identified. The two realistic responses considered are the use of a spacecraft functioning as either a kinetic impactor or a nuclear explosive carrier to deflect the approaching NEO. The choice depends on the NEO size and mass, the available response time prior to Earth impact, and the various uncertainties. Whenever practical, the kinetic impactor is the preferred approach, but various factors, such as large uncertainties or short available response time, reduce the kinetic impactor's suitability and, ultimately, eliminate its sufficiency. Herein we examine response time and the activities that occur between the time when an NEO is recognized as being a sufficient threat to require a deflection and the time when the deflection impulse is applied to the NEO. To use a kinetic impactor for successful deflection of an NEO, it is essential to minimize the reaction time and maximize the time available for the impulse delivered to the NEO by the kinetic impactor to integrate forward in time to the eventual deflection of the NEO away from Earth impact. To shorten the response time, we develop tools to survey the profile of needed spacecraft launches and the possible mission payloads. We further present a vehicle design capable of either serving as a kinetic impactor, or, if the need arises, serving as a system to transport a nuclear explosive to the NEO. These results are generated by analyzing a specific case study in which the simulated Earth-impacting NEO is modeled very closely after the real NEO known as 101955 Bennu (1999 RQ36). Bennu was selected for our case study in part because it is the best-studied of the known NEOs. It is also the destination of NASA's OSIRIS-REx sample return mission, which is, at the time of this writing, enroute to Bennu following a September 2016 launch.
Document ID
20205000654
Acquisition Source
Goddard Space Flight Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Brent W. Barbee
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Megan Bruck Syal
(Lawrence Livermore National Laboratory Livermore, California, United States)
David Dearborn
(Lawrence Livermore National Laboratory Livermore, California, United States)
Galen Gisler
(Los Alamos National Laboratory Los Alamos, New Mexico, United States)
Kevin Greenaugh
(United States Department of Energy Washington D.C., District of Columbia, United States)
Kirsten M. Howley
(Lawrence Livermore National Laboratory Livermore, California, United States)
Ron Leung
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Josh Lyzhoft
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Paul L Miller
(Lawrence Livermore National Laboratory Livermore, California, United States)
Joseph A Nuth
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Catherine Plesko
(Los Alamos National Laboratory Los Alamos, New Mexico, United States)
Bernard D. Seery
(Universities Space Research Association Columbia, Maryland, United States)
Joseph Wasem
(Lawrence Livermore National Laboratory Livermore, California, United States)
Robert P. Weaver
(Los Alamos National Laboratory Los Alamos, New Mexico, United States)
Melak Mekonen Zebenay
(Science Applications International Corporation (United States) McLean, Virginia, United States)
Date Acquired
April 8, 2020
Publication Date
December 22, 2017
Publication Information
Publication: Acta Astronautica
Publisher: Elsevier
Volume: 143
Issue Publication Date: February 1, 2018
ISSN: 0094-5765
Subject Category
Astronautics (General)
Funding Number(s)
WBS: 582622.02.01.02.46
CONTRACT_GRANT: NNH14ZDA001NSSO
CONTRACT_GRANT: DEAC52-07NA27344
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
External Peer Committee
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