Method for controlling the pressure and a mixture ratio of a rocket engine, and corresponding device
A rocket engine, mixture technology, applied in the direction of rocket engine installation, engine control, machine/engine, etc.
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[0041] Methods and apparatus for controlling pressure and mixture ratio within a rocket motor are described next.
[0042] figure 1 A system including a control device DC and a rocket motor is shown. Although the rocket engine in this figure is included in the system of the invention, its internal structure has no say in the invention itself.
[0043] by instructing, figure 1 The structure of the engine in corresponds to that described in more detail in document EP 2187031.
[0044] In this embodiment, the engine has two propellant containers 131 and 132 . Downstream of each container 131 and 132, the engine has a respective pump 111 or 112.
[0045] Downstream of the pump, the engine has two control valves VR1 and VR2, called "bypass" valves, and located on the two turbine lines. It can be observed that in this specification, reference numerals VR1 and VR2 are used both to designate control valves and to control signals for determining their positions.
[0046] The engi...
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