| 摘要 |
In a combustion chamber (5) of a liquid propellant engine (1), a combustible liquid and an oxidising mixture are fed by means of two different independent and mechanically separate feed pumps (12),(27) and driven by respective turbines (16),(32) which are also independent and mechanically separate from each other; the oxidising mixture generated by a combustible liquid pre-burner (22) passing through one of the turbines (32); and the heated combustible liquid passing through the other turbine (16) before it is supplied to the combustion chamber (5); the oxidising mixture, after having passed through the respective turbine (32), flows into the combustion chamber (5) via an injection plate (6). |
