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- W3048870990 abstract "During spacecraft reentry into earth atmosphere, it has to encounter wide range of Mach numbers varying from hypersonic to subsonic. For safety of the payload/crew, vehicle structure should be maintained within certain temperature limits. Further, there are significantly high deceleration levels on the body. In the present work, software package is developed which carries out multi-disciplinary analysis (MDA) of axi-symmetric reentry vehicle configuration with trajectory and aerodynamic heating as two participating disciplines. The geometry parameters and initial conditions are perturbed for ballistic and semi-ballistic entries, and their influence is seen on reentry trajectory and aerodynamic heating rates. This work is useful for quick assessment of the data for various configurations during reentry vehicle’s initial design phase." @default.
- W3048870990 created "2020-08-18" @default.
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- W3048870990 date "2020-01-01" @default.
- W3048870990 modified "2023-09-27" @default.
- W3048870990 title "Multi-disciplinary Analysis of a Reentry Vehicle" @default.
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- W3048870990 doi "https://doi.org/10.1007/978-981-15-5432-2_2" @default.
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