Combustion-mode transition of a solid propellant rocket motor by nitrogen gas injection and combustion gas release.
| Autor: | Masafumi Tanaka1 osc999@jcom.home.ne.jp, Masashi Yamakami1, Taku Sakaguchi1, Shogo Bando1, Ryusuke Wada1, Takahiro Ito1, Toshihito Ito1, Yuta Kajiya1 |
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| Zdroj: | Science & Technology of Energetic Materials. 2022, Vol. 83 Issue 6, p163-168. 6p. |
| Databáze: | Academic Search Ultimate |
| Externí odkaz: |
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