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...

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Bibliographic Details
Main Authors: Kazuhisa CHIBA, Shin'ya WATANABE, Masahiro KANAZAKI, Koki KITAGAWA, Toru SHIMADA
Format: Article
Language:Japanese
Published: The Japan Society of Mechanical Engineers 2014-10-01
Series:Nihon Kikai Gakkai ronbunshu
Subjects:
Online Access:https://www.jstage.jst.go.jp/article/transjsme/80/818/80_2014trans0287/_pdf/-char/en