Fuel regression behavior of swirling-injection end-burning hybrid rocket engine

Fuel regression behavior of swirling-injection end-burning hybrid rocket engine

Burning experiments were conducted to better understand the fuel regression behavior in a swirling-injection end-burning hybrid rocket engine using paraffin wax/gaseous oxygen propellant. The oxidizer mass flow rate, grain diameter, and the distance between the oxidizer injector and the grain end-su...

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Bibliographic Details
Main Authors: Takashi SAKURAI, Yuya OISHIGE, Kazuyuki SAITO
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2019-12-01
Series:Journal of Fluid Science and Technology
Subjects:
swirling-injection
end-burning
fuel regression rate
hybrid rocket engine
Online Access:https://www.jstage.jst.go.jp/article/jfst/14/3/14_2019jfst0025/_pdf/-char/en

Internet

https://www.jstage.jst.go.jp/article/jfst/14/3/14_2019jfst0025/_pdf/-char/en

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