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载人登月运载火箭总体方案研究

蔡益飞

上海航天2012,Vol.29Issue(4):1-6,6.
上海航天2012,Vol.29Issue(4):1-6,6.

载人登月运载火箭总体方案研究

Research on General Scheme of Launch Vehicle for Manned Lunar Mission

蔡益飞1

作者信息

  • 1. 上海航天技术研究院,上海201109
  • 折叠

摘要

Abstract

The characteristic and performance of the scheme of the heavy launch vehicle in aboard were introduced in this paper. The four suggestions for the development of the engine of the new generation launch vehicle in China were put forward, such as the configuration with two and half stage was the first choice, the thrust with thrust 120, 140 t could satisfy the requirement of the first stage of the future launch vehicle in China, the hydrogen-oxygen engine with vacuum thruster 100 t was the right choice in China, and the suitable maximum diameter of the vehicle was 7-8 m. The developing routes of the heavy launch vehicle were given out aiming to the manned lunar mission task in China. One configuration was optimazed and the some detail design was made.

关键词

航天运输/载人登月/重型运载火箭

Key words

Aerospace transportation/Manned moon landing/Heavy launch vehicle

引用本文复制引用

蔡益飞..载人登月运载火箭总体方案研究[J].上海航天,2012,29(4):1-6,6.

上海航天

2096-8655

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