Damage mechanics - based creep - fatigue analysis of combustion chamber for satellite's bipropellant thruster
Creep - fatigue analyses based on the concept of continuum damage mechanics were conducted for the combustion chamber used in a satellite's bipropellant thruster. The previously identified models and material parameters for the niobium alloy (C103) which is used as the combustion chamber&am...
| Main Authors: | , , |
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| Format: | Article |
| Language: | Japanese |
| Published: |
The Japan Society of Mechanical Engineers
2016-02-01
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| Series: | Nihon Kikai Gakkai ronbunshu |
| Subjects: | |
| Online Access: | https://www.jstage.jst.go.jp/article/transjsme/82/835/82_15-00667/_pdf/-char/en |