Conceptual design: Dependence of parameterization on design performance of three-stage hybrid rocket

Conceptual design: Dependence of parameterization on design performance of three-stage hybrid rocket

The subject of this paper is to improve on parameterization for conceptual design method of three stage hybrid rocket. Multi-Objective Genetic Algorithm (MOGA) is employed to solve multi-disciplinary design exploration of a three-stage launch vehicle concept using a hybrid rocket engine. MOGA which...

Full description

Bibliographic Details
Main Authors: Masahiro KANAZAKI, Fumio KANAMORI, Yosuke KITAGAWA, Masaki NAKAMIYA, Koki KITAGAWA, Toru SHIMADA
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2014-11-01
Series:Journal of Fluid Science and Technology
Subjects:
hybrid rocket
multidisciplinary design optimization
genetic algorithm
conceptual design
design parameterization
Online Access:https://www.jstage.jst.go.jp/article/jfst/9/5/9_2014jfst0071/_pdf/-char/en

Internet

https://www.jstage.jst.go.jp/article/jfst/9/5/9_2014jfst0071/_pdf/-char/en

Similar Items