Rocket Engine with Continuous Detonation Combustion of the Natural Gas--Oxygen Propellant System.
| Autor: | Frolov, S. M.1,2,3 smfrol@chph.ras.ru, Aksenov, V. S.1,2,3, Ivanov, V. S.1,3, Medvedev, S. N.1,3, Shamshin, O.1,2,3, Yakovlev, N. N.4, Kostenko, I. I.4 |
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| Zdroj: | Doklady Physical Chemistry. Feb2018, Vol. 478 Issue 2, p31-34. 4p. |
| Databáze: | Academic Search Ultimate |
| Externí odkaz: |
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