A rechargeable gas-storage solid propellant power plant
A solid propellant and power device technology, applied in jet propulsion devices, rocket engine devices, machines/engines, etc., can solve problems such as separation difficulties, achieve simple ignition methods, high system reliability, and save structural materials.
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[0029] The idea, specific structure and technical effects of the present invention will be further described below in conjunction with the accompanying drawings and embodiments, so as to understand the purpose, features and effects of the present invention.
[0030] Such as figure 1 As shown, a reloaded gas-storage solid rocket motor includes: charge storage chamber rotating motor 1, first charge push rod 2, charge storage chamber 3, second charge push rod 4, pulse charge 5. Main charge 6, charge loader 7, residual gas release device 8, gas storage chamber 9, pressure measurement and control device 10, igniter 11, nozzle seal 12, valve control nozzle 13. The remaining gas release device 8 is connected to the charge loader 7 through a pipeline, the opening at the front head of the gas storage chamber 9 is connected to the charge loader 7 to form a closed space, and the tail is connected to the controllable nozzle 13 . The main charge 6 is designed as an internal combustion tub...
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