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Wang Zhongwei; Zhang Weihua; Hu Xiaoping;Wang Zhenguo(National University of Defense Technology, Changsha 410073)
Published:
Abstract: ffect of arrangements of a pressure-feed, liquid propellant space engines system on centroid drift of a spacecraft was studied in this paper. A mathmematical model for calculation of the centroid drift was given.Some important conclusions of the arrangements for a liquid propellant space engines system were obtained.
Wang Zhongwei; Zhang Weihua; Hu Xiaoping;Wang Zhenguo(National University of Defense Technology, Changsha 410073). EFFECT OF LIQUID PROPELLANT SPACE ENGINES SYSTEM ON CENTROID DRIFT[J]. .
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