Diversity of design knowledge for launch vehicle in view of fuels on hybrid rocket engine

A single-stage launch vehicle with hybrid rocket engine, which uses solid fuel and liquid oxidizer, has been studied and developed as a next-generation rocket for scientific observation due to the advantages as low cost, safety, re-ignition, and reduced pollution. Thereupon, the knowledge regarding...

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Bibliographic Details
Main Authors: Kazuhisa CHIBA, Masahiro KANAZAKI, Masaki NAKAMIYA, Koki KITAGAWA, Toru SHIMADA
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2014-07-01
Series:Journal of Advanced Mechanical Design, Systems, and Manufacturing
Subjects:
Online Access:https://www.jstage.jst.go.jp/article/jamdsm/8/3/8_2014jamdsm0023/_pdf/-char/en