Interval statistic based reliability analysis method on small sample hot test of satellite thruster-Reference-Cited by-同舟云学术

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Interval statistic based reliability analysis method on small sample hot test of satellite thruster

Published:2018-08 Issue: Volume:60 Page:581-591
ISSN:0307-904X
Container-title:Applied Mathematical Modelling
language:en
Short-container-title:Applied Mathematical Modelling

Author:

Cui Yi^ORCID,Zhang Yongbo^ORCID,Wang Zhihua^ORCID,Fu Huimin,Mao Xiaofang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Applied Mathematics,Modeling and Simulation

Reference42 articles.

1. Reliability assessment of 12 N bipropellant thruster system for geostationary satellite;Lin,2013

2. Spacecraft Reliability and Multi-State Failures: A Statistical Approach;Saleh,2011

3. Further improvements and qualification status of Astrium's 10 N bipropellant thruster family;Schulte,2003

4. Development of a 10-N liquid bipropellant thruster for geostationary spacecraft program of Indian Space Reseach Organisation;Balan,2009

5. Satellite and satellite subsystems reliability: statistical data analysis and modeling;Castet;Reliab. Eng. Syst. Saf.,2009

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