Author:
TATEYAMA Tetsuya,TAKANO Atsushi
Publisher
Japan Society for Aeronautical and Space Sciences
Reference6 articles.
1. 1) HyperTEK® Hybrid Rocket Propulsion Systems, http://www.hypertekhybrids.com/manual.pdf （最終閲覧日：2018年9月20日）
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3. Fuel Regression Characteristics of Cascaded Multistage Impinging-Jet (CAMUI) Type Hybrid Rocket
4. A Preliminary Study of End-Burning Hybrid Rocket. Part 1. Combustion Stability.
5. The Launch Test of the Hybrid Rocket and Its Range Safety
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