Optimal two-stage parachute and retro motor sizing for launch vehicle stage recovery

A deceleration system consisting of staged parachute clusters and retro thrusters is optimized for the recovery of the first stage of a launch vehicle on sea. Optimal mass as well as reduction in speed by each parachute cluster and the retro thrusters is essential to minimize the inherent payload lo...

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Veröffentlicht in:	Sadhana (Bangalore) Jg. 45; H. 1
Hauptverfasser:	Priyadarshi, Pankaj, Joseph, Leya, Saroha, Kamal
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New Delhi Springer India 01.12.2020 Springer Nature B.V
Schlagworte:	Clusters Deceleration Degrees of freedom Design optimization Engineering Evolutionary algorithms Grain design High thrust Initial conditions Launch vehicles Multidisciplinary design optimization Multiple objective analysis Parachutes Pareto optimization Pareto optimum Recovery Rockets Spacecraft components Thrusters A parachute cluster Multidisciplinary design optimization (MDO) multi-objective evolutionary algorithm (MOEA) MOEA DO stage recovery solid motor grain design multiobjective multidisciplinary design optimization (M three degrees of freedom (3-DOF) trajectory simulations
ISSN:	0256-2499, 0973-7677
Online-Zugang:	Volltext
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