Manned space flight launch vehicle CZ-2F rliability growth management

Author

Liu, Xin ; Li, Wenzhao ; Wang, Yinghao

Author_Institution

Quality Dept., China Acad. of Launch Vehicle Technol. Syst. Eng., Beijing, China

fYear

2009

fDate

20-24 July 2009

Firstpage

378

Lastpage

381

Abstract

This paper introduces that launch vehicle CZ-2F which take on the Chinese Manned Space Flight Engineering make use of reliability growth management reasonably from development to Y7. Engineer not only control the risk which is brought from applying new technology, but also enhance reliability from CZ-2E 0.91 to Y7 0.9807 by applying reliability design, reliability analysis, reliability test and electric component control again and again. CZ-2F reliability growth supported Chinese Manned Space Flight Engineering to success effectively, and made a pattern to promote next step development of Chinese Manned Space Flight Engineering.

Keywords

aerospace engineering; reliability; space vehicles; Chinese Manned Space Flight Engineering; manned space flight launch vehicle CZ-2F; reliability design; reliability growth management; Aerospace engineering; Automotive engineering; Design engineering; Engineering management; Reliability engineering; Risk analysis; Risk management; Space technology; Space vehicles; Technology management; CZ-2F; Manned Space Flight; reliability growth management;

fLanguage

English

Publisher

ieee

Conference_Titel

Reliability, Maintainability and Safety, 2009. ICRMS 2009. 8th International Conference on

Conference_Location

Chengdu

Print_ISBN

978-1-4244-4903-3

Electronic_ISBN

978-1-4244-4905-7

Type

conf

DOI

10.1109/ICRMS.2009.5270169

Filename

5270169