Failure mechanism and life evaluation of liquid rocket engine combustion chamber under severe multi-physics conditions
In Japan, new developments of liquid rocket engines are now underway for Japan's next flagship launch system. In the development, front-loading design process is applied to reduce development costs and to increase reliability. Therefore it is indispensable to precisely evaluate life time of...
Main Authors: | Miki NISHIMOTO, Hideyo NEGISHI, Shinobu YOSHIMURA, Naoto KASAHARA, Hiroshi AKIBA, Hideo SUNAKAWA, Shusuke HORI, Nobuki NEGORO |
---|---|
Format: | Article |
Language: | Japanese |
Published: |
The Japan Society of Mechanical Engineers
2015-05-01
|
Series: | Nihon Kikai Gakkai ronbunshu |
Subjects: | |
Online Access: | https://www.jstage.jst.go.jp/article/transjsme/81/826/81_14-00674/_pdf/-char/en |
Similar Items
-
Development of rocket motor with ceramic insulator in combustion chamber /
by: Muhammad Nurizad Rosli, 1988-, et al.
Published: (2010) -
Development of rocket motor with ceramic insulator in combustion chamber [electronic resource] /
by: Muhammad Nurizad Rosli, 1988-
Published: (2010) -
Original Romanian Research for a Rocket Engine with Multiple Combustion Chambers during 1940 - 1944
by: Nicolae-Florin ZAGANESCU, et al.
Published: (2020-03-01) -
Liquid rocket combustion chamber acoustic characterization
by: Cândido Magno de Souza, et al.
Published: (2010-09-01) -
Comprehensive modeling of a liquid rocket combustion chamber/
by: 299929 Liang, Pak-Yan, et al.
Published: (1985)