Structural impact simulation using program Krash

Use 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 v...

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Main Author: Liaw, J. C.
Format: Report
Language:English
Published: 1992
Subjects:
Online Access:http://hdl.handle.net/1826/245
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spelling ftcranfield:oai:dspace.lib.cranfield.ac.uk:1826/245 2024-06-09T07:49:36+00:00 Structural impact simulation using program Krash Liaw, J. C. 1992 1963 bytes 819518 bytes text/plain application/pdf http://hdl.handle.net/1826/245 en_UK eng College of Aeronautics Report;9010 CIT/CoA/R;9010 http://hdl.handle.net/1826/245 Technical Report 1992 ftcranfield 2024-05-10T03:08:38Z Use 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. Use 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. This 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). CIT Report South pole Cranfield University: Collection of E-Research - CERES South Pole
institution Open Polar
collection Cranfield University: Collection of E-Research - CERES
op_collection_id ftcranfield
language English
description Use 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. Use 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. This 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). CIT
format Report
author Liaw, J. C.
spellingShingle Liaw, J. C.
Structural impact simulation using program Krash
author_facet Liaw, J. C.
author_sort Liaw, J. C.
title Structural impact simulation using program Krash
title_short Structural impact simulation using program Krash
title_full Structural impact simulation using program Krash
title_fullStr Structural impact simulation using program Krash
title_full_unstemmed Structural impact simulation using program Krash
title_sort structural impact simulation using program krash
publishDate 1992
url http://hdl.handle.net/1826/245
geographic South Pole
geographic_facet South Pole
genre South pole
genre_facet South pole
op_relation College of Aeronautics Report;9010
CIT/CoA/R;9010
http://hdl.handle.net/1826/245
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