Optimal transfers of spacecraft with bimodal propulsion

被引：0

作者：

Kiforenko B.N. ^{[1
]}

Kharitonov A.M. ^{[2
]}

机构：

[1] S. P. Timoshenko Institute of Mechanics, National Academy of Sciences of Ukraine, Kyiv 03057

[2] T. Shevchenko National University, Kyiv 01601, 2 Glushkova St., GSP

来源：

International Applied Mechanics | 2011年 / 46卷 / 10期

关键词：

Bimodal nuclear termal rocket engine; Necessary optimality conditions; Optimal interplanetary transfer;

D O I：

10.1007/s10778-011-0408-7

中图分类号：

学科分类号：

摘要：

An optimization problem for the interplanetary transfer of a spacecraft with bimodal nuclear rocket engine is formulated. The transfer trajectory combines high- and low-thrust phases. The necessary optimality conditions are analyzed. The solution for a 180-day Earth-Mars transfer is presented. © 2011 Springer Science+Business Media, Inc.

引用

页码：1154 / 1163

页数：9

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