Retrievable electric rocket used for intercepting small aircrafts
A return type, electric power technology, applied in the field of aircraft, can solve the problems of high use cost, short effective distance, slow capture speed, etc., and achieve the effect of strong applicability and low use cost
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[0025] A returnable electro-powered rocket for intercepting small aircraft, such as figure 1 , figure 2 , image 3 As shown, it includes fairing 1, distance sensor 2, rocket shell 3, wing arm 4, air inlet 5, rocket wing 6, tail rudder motor 7, tail rudder 8, connecting rib 9, image recognizer 10, capture Net 11, high-pressure air chamber 12, electrical control chamber 13, release valve 14, partition 15, first plane joint 16, second plane joint 17, third plane joint 18, pull rod 19, pull plate 20, lead screw 21, Lead screw drive motor 22, motor support 23, secondary thrust motor 24, secondary propeller 25, primary thrust motor 26, primary propeller 27 and return spring 28.
[0026] The external structure of the returnable electric powered rocket is: the top of the cylindrical rocket shell 3 is plugged with a conical fairing 1, and the fairing 1 and the rocket shell 13 are connected by a return spring 28; A distance sensor 2 and an image recognition device 10 are symmetrical...
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