A theoretical study on throttle ranges of O/F controllable hybrid rocket propulsion systems

The characteristics of several O/F control methods for hybrid rocket propulsion have been discussed and theoretically analyzed from the physical properties of propellants and fuel regression behavior. In this research, comparisons have been made among different oxidizer injection methods of Altering...

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Bibliographic Details
Main Authors: Kohei OZAWA, Toru SHIMADA
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2018-11-01
Series:Journal of Fluid Science and Technology
Subjects:
Online Access:https://www.jstage.jst.go.jp/article/jfst/13/4/13_2018jfst0031/_pdf/-char/en