Nuclear subsurface explosion modeling and hydrodynamic fragmentation simulation of hazardous asteroids

dc.contributor.advisor Bong Wie
dc.contributor.author Premaratne, Pavithra
dc.contributor.department Aerospace Engineering
dc.date 2018-08-11T06:37:38.000
dc.date.accessioned 2020-06-30T02:52:36Z
dc.date.available 2020-06-30T02:52:36Z
dc.date.copyright Wed Jan 01 00:00:00 UTC 2014
dc.date.embargo 2001-01-01
dc.date.issued 2014-01-01
dc.description.abstract <p>Disruption and fragmentation of an asteroid using nuclear explosive devices (NEDs) is a highly complex yet a practical solution to mitigating the impact threat of asteroids with short warning time. A Hypervelocity Asteroid Intercept Vehicle (HAIV) concept, developed at the Asteroid Deflection Research Center (ADRC), consists of a primary vehicle that acts as kinetic impactor and a secondary vehicle that houses NEDs. The kinetic impactor (lead vehicle) strikes the asteroid creating a crater. The secondary vehicle will immediately enter the crater and detonate its nuclear payload creating a blast wave powerful enough to fragment the asteroid.</p> <p>The nuclear subsurface explosion modeling and hydrodynamic simulation has been a challenging research goal that paves the way an array of mission critical information. A mesh-free hydrodynamic simulation method, Smoothed Particle Hydrodynamics (SPH) was utilized to obtain both qualitative and quantitative solutions for explosion efficiency. Commercial fluid dynamics packages such as AUTODYN along with the in-house GPU accelerated SPH algorithms were used to validate and optimize high-energy explosion dynamics for a variety of test cases. Energy coupling from the NED to the target body was also examined to determine the effectiveness of nuclear subsurface explosions. Success of a disruption mission also depends on the survivability of the nuclear payload when the secondary vehicle approaches the newly formed crater at a velocity of 10 km/s or higher. The vehicle may come into contact with debris ejecting the crater which required the conceptual development of a Whipple shield. As the vehicle closes on the crater, its skin may also experience extreme temperatures due to heat radiated from the crater bottom. In order to address this thermal problem, a simple metallic thermal shield design was implemented utilizing a radiative heat transfer algorithm and nodal solutions obtained from hydrodynamic simulations.</p>
dc.format.mimetype application/pdf
dc.identifier archive/lib.dr.iastate.edu/etd/13852/
dc.identifier.articleid 4859
dc.identifier.contextkey 5777564
dc.identifier.doi https://doi.org/10.31274/etd-180810-2319
dc.identifier.s3bucket isulib-bepress-aws-west
dc.identifier.submissionpath etd/13852
dc.identifier.uri https://dr.lib.iastate.edu/handle/20.500.12876/28039
dc.language.iso en
dc.source.bitstream archive/lib.dr.iastate.edu/etd/13852/Premaratne_iastate_0097M_14269.pdf|||Fri Jan 14 20:02:31 UTC 2022
dc.subject.disciplines Aerospace Engineering
dc.title Nuclear subsurface explosion modeling and hydrodynamic fragmentation simulation of hazardous asteroids
dc.type article
dc.type.genre thesis
dspace.entity.type Publication
relation.isOrgUnitOfPublication 047b23ca-7bd7-4194-b084-c4181d33d95d
thesis.degree.level thesis
thesis.degree.name Master of Science
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