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Near Earth asteroid orbit perturbation and fragmentationCollisions by near earth asteroids or the nuclei of comets pose varying levels of threat to man. A relatively small object, approximately 100 meter diameter, which might be found on an impact trajectory with a populated region of the Earth, could potentially be diverted from an Earth impacting trajectory by mass driver rocket systems. For larger bodies, such systems would appear to be beyond current technology. For any size object, nuclear explosions appear to be more efficient, using either the prompt blow-off from neutron radiation, the impulse from ejecta of near-surface explosion for deflection, or as a fragmenting charge. Practical deflections of bodies with diameters of 0.1, 1, and 10 km require interception, years to decades prior to earth encounter, with explosions a few kilotons, megatons, or gigatons, respectively, of equivalent TNT energy to achieve orbital velocity changes or destruction to a level where fragments are dispersed to harmless spatial densities.
Document ID
19920011112
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ahrens, Thomas J.
(California Inst. of Tech. Pasadena., United States)
Harris, Alan W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
March 18, 1992
Subject Category
Astrophysics
Report/Patent Number
NASA-CR-190116
NAS 1.26:190116
Report Number: NASA-CR-190116
Report Number: NAS 1.26:190116
Accession Number
92N20354
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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