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载人登月飞行方案研究

彭祺擘 李桢 李海阳

上海航天2012,Vol.29Issue(5):14-19,72,7.
上海航天2012,Vol.29Issue(5):14-19,72,7.

载人登月飞行方案研究

Analysis on Manned Lunar Mission Flight Mode

彭祺擘 1李桢 1李海阳1

作者信息

  • 1. 国防科学技术大学航天与材料工程学院,湖南长沙410073
  • 折叠

摘要

Abstract

According to different location of rendezvous nodes with or without the earth orbit or lunar orbit, the lunar route was divided in to four baseline lunar mission modes in this paper, which were earth orbit rendezvous (EOR)-lunar orbit rendezvous (LOR), EOR-direct return, LOR, and direct-direct. The various approaches for each mode were analyzed. The mass of manned lunar mission and the requirement of launch vehicle were discussed. The launch windows and mission schemes of the one-launch, two-launch and assembled in lunar orbit or earth orbit were studied. The suggestions were put forward. The study was useful to the scheme determination of China's manned lunar mission.

关键词

载人登月/交会对接/运载火箭/发射窗口

Key words

Manned lunar mission/Rendezvous and dock/Launch vehicle/Launch window

引用本文复制引用

彭祺擘,李桢,李海阳..载人登月飞行方案研究[J].上海航天,2012,29(5):14-19,72,7.

基金项目

中国载人航天工程办公室载人登月概念研究项目 ()

上海航天

2096-8655

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