Conceptual design of single-stage launch vehicle with hybrid rocket engine using design informatics
A single-stage launch vehicle with hybrid rocket engine has been conceptually designed by using design informatics, which has three points of view, i.e., problem definition, optimization, and data mining. The primary objective of the present design is that the down range and the duration time in the...
Main Authors: | Kazuhisa CHIBA, Shin'ya WATANABE, Masahiro KANAZAKI, Koki KITAGAWA, Toru SHIMADA |
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Format: | Article |
Language: | Japanese |
Published: |
The Japan Society of Mechanical Engineers
2014-10-01
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Series: | Nihon Kikai Gakkai ronbunshu |
Subjects: | |
Online Access: | https://www.jstage.jst.go.jp/article/transjsme/80/818/80_2014trans0287/_pdf/-char/en |
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