A Preliminary Parameter Analysis on the Speed Reduction Scheme of the Retro-Rocket Used by Re-entry Capsule | |||||
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With the development of deep-space exploration, the size of manned spaceship increases, the mass of re-entry capsule is getting heavier, and the speed reduction which relies on the parachute becomes more difficult. Based on the study of other countries’ development of manned spaceship, this pa (Editor : 系统管理员) | |||||