Development of the fuel heating device for the component test of aerospace propulsion systems

For the next generation space launch vehicle, fully reusable spaceplane with rocket and ramjet combined propulsion system is proposed. That type of spaceplane can drastically reduce the cost per unit mass of the payload. One of the main technical challenges of the spaceplane is the propulsion system...

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Bibliographic Details
Main Authors: Mitsuhiro SOEJIMA, Kiyoshi NOJIMA, Sadatake TOMIOKA, Noboru SAKURANAKA
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2016-02-01
Series:Journal of Fluid Science and Technology
Subjects:
Online Access:https://www.jstage.jst.go.jp/article/jfst/11/1/11_2016jfst0006/_pdf/-char/en