Optimization of the propulsion for multistage solid rocket motor launchers

被引：10
|
作者：
Calabro, M [1 ]
Dufour, A [1 ]
Macaire, A [1 ]
机构：
[1] EADS Launch Vehicles, F-78133 Les Mureaux, France
来源：
ACTA ASTRONAUTICA | 2002年 / 50卷 / 04期
关键词：
Multistage solid rocket motor launchers;
D O I：
10.1016/S0094-5765(01)00164-3
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Some tools focused on a rapid multidisciplinary optimization capability for multistage launch vehicle design were developed at EADS-LV. These tools may be broken down into two categories, those related to propulsion design optimization and a computer code devoted to trajectories and under constraints optimization. Both are linked in order to obtain optimal vehicle design after,an iterative process. After a description of the two categories tools, an example of application is given on a small space launcher. (C) 2002 International Astronautical Federation. Published by Elsevier Science Ltd. All rights reserved.
引用
收藏
页码：201 / 208
页数：8
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