The Propulsion System of Shenzhou 13 Manned Spaceship

doi:10.3969/j.issn.1671-0940.2022.01.004

AEROSPACE CHINA ›› 2022, Vol. 23 ›› Issue (1): 27-32.doi: 10.3969/j.issn.1671-0940.2022.01.004

The Propulsion System of Shenzhou 13 Manned Spaceship

出版日期:2022-07-20 发布日期:2022-07-20

The Propulsion System of Shenzhou 13 Manned Spaceship

Shanghai Institute of Space Propulsion, Shanghai 201112

Online:2022-07-20 Published:2022-07-20
About author:GU Shuaihua (1982− ), received his Master’s degree from the Nanjing University of Aeronautics and Astronautics. He is now mainly engaged in the propulsion system of manned spacecraft.

摘要/Abstract

Abstract: Based on the requirements of manned spaceships, this paper introduces the characteristics of the propulsion system from the perspectives of design scheme, basic composition, safety and reliability measures, and also introduces the ground test verification and on-orbit flight characteristics of the Shenzhou 13 propulsion system. According to the flight results, it was seen that the performance of the Shenzhou 13 propulsion system fully met the engineering requirements for the manned space mission.

Key words:

manned spaceflight, Shenzhou 13 spaceship, propulsion system

The Propulsion System of Shenzhou 13 Manned Spaceship

[J]. AEROSPACE CHINA, 2022, 23(1): 27-32.

GU Shuaihua, LU Fei.

The Propulsion System of Shenzhou 13 Manned Spaceship

[J]. AEROSPACE CHINA, 2022, 23(1): 27-32.

ISSN 1671-0940

CN 11-4673/V

The Propulsion System of Shenzhou 13 Manned Spaceship

The Propulsion System of Shenzhou 13 Manned Spaceship

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