Determination of damage area of spacecraft shields impacted by space debris at hypervelocity using an SPH mesh.

dc.contributor.authorBhargavi, S.S.
dc.contributor.authorSoschinske, Kurt A.
dc.contributor.authorLankarani, Hamid M.
dc.date.accessioned2007-09-17T14:40:48Z
dc.date.available2007-09-17T14:40:48Z
dc.date.issued2007-04-27
dc.descriptionPaper presented to the 3rd Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at the Hughes Metropolitan Complex, Wichita State University, April 27, 2007.en
dc.descriptionResearch completed Department of Mechanical Engineering, College of Engineeringen
dc.description.abstractSpace debris, are objects in Earth orbit consisting of small fragments from spent rocket stages and non-functional satellites. Accumulated in the lower earth orbit, these often cause considerable damage to the spacecraft orbiting around the earth. Hence it’s necessary to develop ways to protect the newly placed spacecraft from the debris. The goal of the project was to determine the damage area of the pressure wall using the Smoothed Particle Hydrodynamic (SPH) meshing, a dynamic finite element modeling (FEM) method.en
dc.format.extent178428 bytes
dc.format.mimetypeapplication/pdf
dc.identifier.citationBhargavi, S.S., Soschinske, K.A. & Lankarani, H. (2007). Determination of damage area of spacecraft shields impacted by space debris at hypervelocity using an SPH mesh. In Proceedings : 3rd Annual Symposium : Graduate Research and Scholarly Projects. Wichita, KS : Wichita State University, p.217-218en
dc.identifier.urihttp://hdl.handle.net/10057/918
dc.language.isoen_USen
dc.publisherWichita State University. Graduate School.en
dc.relation.ispartofseriesGRASPen
dc.relation.ispartofseriesv.3en
dc.titleDetermination of damage area of spacecraft shields impacted by space debris at hypervelocity using an SPH mesh.en
dc.typeConference paperen
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