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Los Alamos RAGE Simulations of the HAIV Mission ConceptThe mitigation of potentially hazardous objects (PHOs) can be accomplished by a variety of methods including kinetic impactors, gravity tractors and several nuclear explosion options. Depending on the available lead time prior to Earth impact, non- nuclear options can be very effective at altering a PHOs orbit. However if the warning time is short nuclear options are generally deemed most effective at mitigating the hazard. The NIAC mission concept for a nuclear mission has been presented at several meetings, including the last PDC (2013).We use the adaptive mesh hydrocode RAGE to perform detailed simulations of this Hypervelocity Asteroid Intercept Vehicle (HAIV) mission concept. We use the RAGE code to simulate the crater formation by the kinetic impactor as well as the explosion and energy coupling from the follower nuclear explosive device (NED) timed to detonate below the original surface to enhance the energy coupling. The RAGE code has been well validated for a wide variety of applications. A parametric study will be shown of the energy and momentum transfer to the target 100 m diameter object: 1) the HAIV mission as planned; 2) a surface explosion and 3) a subsurface (contained) explosion; both 2) and 3) use the same source energy as 1).Preliminary RAGE simulations show that the kinetic impactor will carve out a surface crater on the object and the subsequent NED explosion at the bottom of the crater transfers energy and momentum to the target effectively moving it off its Earth crossing orbit. Figure 1 shows the initial (simplified) RAGE 2D setup geometry for this study. Figure 2 shows the crater created by the kinetic impactor and Figure 3 shows the time sequence of the energy transfer to the target by the NED.
Document ID
20150011684
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Weaver, Robert P.
(Los Alamos National Lab. NM, United States)
Barbee, Brent W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Wie, Bong
(Iowa State Univ. Ames, IA, United States)
Zimmerman, Ben
(Iowa State Univ. Ames, IA, United States)
Date Acquired
June 26, 2015
Publication Date
April 13, 2015
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
GSFC-E-DAA-TN22343
IAA-PDC-15-03-14
GSFC-E-DAA-TN22250
Report Number: GSFC-E-DAA-TN22343
Report Number: IAA-PDC-15-03-14
Report Number: GSFC-E-DAA-TN22250
Meeting Information
Meeting: IAA Planetary Defense Conference
Location: Frascati, Roma
Country: Italy
Start Date: April 13, 2015
End Date: April 17, 2015
Sponsors: International Academy of Astronautics, European Space Agency. ESRIN
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Asteroid Mitigation
Deflection Disruption
Hydrocode
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