Computational modelling of aerodynamic disturbances on spacecraft within a concurrent engineering framework
This research was motivated by the need to perform an accurate aerodynamic analysis of the drag deorbit device concept under development within the Space Research Centre, Cranfield University. Its purpose is to deorbit satellites from low Earth orbit at the end of the useful lives, in order to help...
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Main Author | |
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Format | Dissertation |
Language | English |
Published |
Cranfield University
2007
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Online Access | Get full text |
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