Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rocket Using Nitrous Oxide-Reference-Cited by-同舟云学术

Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rocket Using Nitrous Oxide

Published:2022-09 Issue:5 Volume:38 Page:759-770
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Okuda Ryota,Komizu Kodai,Tsuji Ayumu,Miwa Takumi,Fukada Mai,Yokobori Shuichi,Soeda Kentaro,Kamps Landon,Nagata Harunori

Funder

Center of Innovation Program

Japan Society for the Promotion of Science

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B38318

Reference23 articles.

1. ChiaveriniM. J.KuoK. K., Fundamentals of Hybrid Rocket Combustion and Propulsion, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2007, pp. 37–125.

2. A Preliminary Study of End-Burning Hybrid Rocket. Part 1. Combustion Stability.

3. A Preliminary Study of End-Burning Hybrid Rocket. Part 2. Combustion Characteristics.

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