Thermal Protection System and Trajectory Optimization for Orbital Plane Change Aeroassisted Maneuver
http://dx.doi.org/10.5028/jatm.v5i1.208 The aim of this paper was to identify, for a specific maneuver, the optimal combination between the trajectory and the associated heat shield configuration, namely the locations and thicknesses of the ablative and reusable zones, that maximize the allowable p...
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| Format: | Article |
| Language: | English |
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Instituto de Aeronáutica e Espaço (IAE)
2013-03-01
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| Series: | Journal of Aerospace Technology and Management |
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| Online Access: | https://www.jatm.com.br/jatm/article/view/208 |