Actively cooled dual-nozzle strut-plate ejection rocket for rocket-based combined-cycle engine
An ejection rocket and active cooling technology, which is applied to the cooling of engines, combined engines, rocket engine devices, etc., can solve problems such as the harsh environment of ejection rocket engines, achieve reliable cooling, reduce complexity, and reduce flow resistance Effect
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[0022] The present invention is a rocket-based combined cycle engine with active cooling double nozzle support plate ejection rocket, such as figure 1 As shown, the prop ejection rocket body 1 is included, and the prop ejection rocket body 1 is a solid cuboid for longitudinally placing in the isolation section of the engine; the width of the prop ejection rocket body 1 is less than the width of the isolation section, Two independent gas flow passages are formed with the front and rear side walls of the isolation section.
[0023] A vertical combustion chamber 11 is provided near a short side in the prop ejection rocket body 1, and the combustion chamber 11 is a cavity with an open upper end.
[0024] Near the other short side of the combustion chamber 11, there are two vertical Rafal nozzles 4 spaced up and down, communicating with the combustion chamber 11; each Rafal nozzle 4 longitudinally penetrates the support plate to eject the rocket body 1. Its open end communicates w...
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