Structural impact simulation using program Krash

dc.contributor.authorLiaw, J. C.en_UK
dc.date1992en_UK
dc.date.accessioned2005-11-23T12:20:04Z
dc.date.available2005-11-23T12:20:04Z
dc.date.issued1992en_UK
dc.description.abstractUse is made of the KRASH program to simulate a simplified car-into-barrier impact. A step-by-step modelling technique is illustrated whose application at an early stage in the design process, allows an understanding of the contribution of individual components to the overall crash-performance of a vehicle.en_UK
dc.description.abstractUse is made of the KRASH program to simulate a simplified car-into-barrier impact. A step-by-step modelling technique is illustrated whose application at an early stage in the design process, allows an understanding of the contribution of individual components to the overall crash-performance of a vehicle.en_UK
dc.description.abstractThis report is a summary of the group design project of the MSc in Astronautics and Space Engineering at Cranfield University for the year 1996/97. The project was a feasibility study of a European unmanned mission to the lunar south pole to carry out scientific study. The mission proposed uses two spacecraft: (1) an orbiter to take images of the proposed landing site, to measure the Moon’s gravitational field, and to act as a communications relay, and (2) a larger lander which carries a small rover and a crate probe. The orbiter is launched first (if gravity and image data are not already available) so that the lander’s landing site can be selected. The main goal is scientific study of the permanently dark craters at the lunar south pole. The baseline design (developed to the depth of a feasibility study) meets the stated requirements and is comparable to ESA’s medium class missions (cost € 300 M).en_UK
dc.description.sponsorshipCITen_UK
dc.format.extent1963 bytes
dc.format.extent819518 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1826/245
dc.language.isoen_UKen_UK
dc.relation.ispartofseriesCollege of Aeronautics Report;9010en_UK
dc.relation.ispartofseriesCIT/CoA/R;9010en_UK
dc.titleStructural impact simulation using program Krashen_UK
dc.typeTechnical Reporten_UK

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