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Using Information from Rendezvous Missions For Best-Case Appraisals of Impact Damage to Planet Earth Caused By Natural ObjectsThe Asteroid Threat Assessment Project (ATAP), a part of NASAs Planetary Defense Coordination Office (PDCO) has the responsibility to appraise the range of surface damage by potential asteroid impacts on land or water. If a threat is realized, the project will provide appraisals to officials empowered to make decisions on potential mitigation actions. This paper describes a scenario for assessment of surface damage when characterization of an asteroid had been accomplished by a rendezvous mission that would be conducted by the international planetary defense community. It is shown that the combination of data from ground and in-situ measurements on an asteroid provides knowledge that can be used to pin-point its impact location and predict the level of devastation it would cause. The hypothetical asteroid 2017 PDC with a size of 160 to 290 m in diameter to be discussed at the PDC 2017 meeting is used as an example. In order of importance for appraising potential damage, information required is: (1) where will the surface impact occur? (2) What is the mass, shape and size of the asteroid and what is its entry state (speed and entry angle) at the 100 km atmospheric pierce point? And (3) is the asteroid a monolith or a rubble pile? If it is a rubble pile, what is its sub and interior structure? Item (1) is of first order importance to determine levels of devastation (loss of life and infrastructure damage) because it varies strongly on the impact location. Items (2) and (3) are used as input for ATAPs simulations to define the level of surface hazards: winds, overpressure, thermal exposure; all created by the deposition of energy during the objects atmospheric flight, and/or cratering. Topics presented in this paper include: (i) The devastation predicted by 2017 PDCs impact based on initial observations using ATAPs risk assessment capability, (ii) How information corresponding to items (1) to (3) could be obtained from a rendezvous mission, and (iii) How information from a rendezvous mission could be used, along with that from ground observations and data from the literature, could provide input for an new risk analysis capability that is emerging from ATAPs research. It is concluded that this approach would result in appraisal with the least uncertainty possible (herein called the best-case) using simulation capabilities that are currently available or will be in the future.
Document ID
20180000826
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Arnold, James O.
(NASA Ames Research Center Moffett Field, CA, United States)
Chodas, Paul W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ulamec, Stephan
(Deutsches Zentrum fuer Luft- und Raumfahrt e.V. Cologne, Germany)
Mathias, Donovan L.
(NASA Ames Research Center Moffett Field, CA, United States)
Burkhard, Craig D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
January 29, 2018
Publication Date
May 15, 2017
Subject Category
Space Sciences (General)
Aeronautics (General)
Report/Patent Number
ARC-E-DAA-TN42140-1
Meeting Information
Meeting: Annual IAA Planetary Defense Conference (PDC 2017)
Location: Tokyo
Country: Japan
Start Date: May 15, 2017
End Date: May 19, 2017
Sponsors: International Academy of Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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