Novel Mars spacecraft combined propulsion system
A technology of propulsion system and aircraft, applied in power plant type, rocket-type power plant, etc., can solve the problems of carrying a large amount of fuel, unable to meet the mission of Mars aircraft, and achieve the effect of reducing cost
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[0016] Specific implementation method: combined Figure 1 to Figure 3 To illustrate this embodiment: a new type of Mars vehicle combined propulsion system mentioned in this embodiment includes a propeller 1 and a rocket motor 2, and the propeller 1 and rocket motor 2 are installed on the wings of the aircraft 3. Rocket engine 2 comprises oxidant storage tank 4, fuel storage tank 5, oxidant pump 6, fuel pump 7, combustion chamber 8, tail nozzle 9 and flow regulating valve 11; The output end of described oxidant storage tank 4 and fuel storage tank 5 Correspondingly connected to the input ends of the oxidant pump 6 and the fuel pump 7 respectively; flow regulating valves are provided on the pipelines connecting the oxidant storage tank 4 to the oxidant pump 6 and on the pipelines connecting the fuel storage tank 5 to the fuel pump 7 11. The fuel in the oxidant storage tank 4 and the fuel storage tank 5 is delivered to the combustion chamber 8 for combustion through the oxidant p...
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