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Analytical and numerical re-entry analysis of simple-shaped objects
Institution:1. DEIMOS Space S.L.U., Ronda de Poniente, 19, 28760 Tres Cantos, Madrid, Spain;2. European Space Agency (ESA), ESOC, Robert-Bosch-Str. 5, 64293, Darmstadt, Germany;3. HTG - Hyperschall Technologie Göttingen GmbH, Am Handweisergraben 13, D-37120, Bovenden, Germany;1. Korea Advanced Institute of Science and Technology (KAIST), 291 Daehak-Ro, Daejeon 34141, Republic of Korea;2. Korea Astronomy and Space Science Institute (KASI), 776 Daedeok-daero, Daejeon 34055, Republic of Korea;1. Korea Advanced Institute of Science and Technology, Daejeon 34141, Republic of Korea;2. Korea Aerospace Research Institute, Daejeon 305-333, Republic of Korea
Abstract:The application of SCARAB (spacecraft atmospheric re-entry and aerothermal break-up) to several re-entry objects within the last years has shown the need of fast methods and easy-to use guidelines for a first assessment of the survival probability for these objects or parts of them. Such methods and guidelines will be also very helpful during the design process of a satellite in order to decide, whether a controlled re-entry had to be foreseen at the end of the lifetime, or an uncontrolled re-entry would be acceptable.Within current studies HTG has developed analytical and numerical methods to analyze the demise of simple-shaped objects like spheres, boxes, and cylinders. In addition, the SCARAB software system has been used to evaluate the shielding effects of concentric shells.This paper presents the analytical and numerical models used within the study and the results which have been achieved, including demise ranges for several object/material combinations. The SCARAB results for shielding effects are presented as well.
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