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Hu Xiaoping ;Wang Zhongwei; Zhang Yulin(Dept. of Aerospace Technology, National Univ. of defence Technology, Changsha, 410073)  
Based on mass models of liquid propellant thrust system, an approach has beenpresented for optimization on locality arrangement of bipropellant attitude control engines. Theoptimization object function is the total mass of thrust system being smallest, under certain totalefficient control impulsion and total efficient control impulsion moment.
【CateGory Index】: V439.7
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