Optimal two-stage parachute and retro motor sizing for launch vehicle stage recovery - Priyadarshi, Pankaj; Joseph, Leya; Saroha, Kamal (Sadhana (Bangalore), 2020)
Keywords: 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