Anti-interception flyer with separation layer and smoke releasing function
An anti-interception and flying object technology, applied in the field of space flight, can solve the problem that flying objects in the air cannot be separated, and achieve the effect of reducing release
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Embodiment 1
[0032] The structure of the anti-interception flying object with separation layer and smoke release function described in the present invention is as follows: figure 1 As shown, it includes a processor 1, a detection module 2, a release module 5, a housing 3, an induction device 6, a separation layer 02 and a power supply 4, wherein the detection module 2 is connected to the processor 1 for use in The detection is performed within a preset range and the detection result is sent to the processor 1; the detection module 2 is a radar or a camera. In this embodiment, the detection module 2 is a radar.
[0033] The release module 5 is used to release smoke, and the release module 5 is connected to the processor 1 via the first switch 71, and the processor 1 controls all the devices according to the received detection result that there is an interceptor target within the predetermined range. The first switch 71 is closed to control the release module 5 to work; in this embodiment, ...
Embodiment 2
[0042] On the basis of Embodiment 1, a separation actuator is provided on the separation layer 02, and the third switch 73 is arranged in the housing 3. When the third switch 73 is closed, the separation actuator The action drives the separation layer 02 to break away from the casing 3 . In this implementation, the separating executive mechanism is the detonating device, that is, the electric detonator.
[0043] As another implementation manner, the third switch 73 is disposed on the separation layer 02 .
Embodiment 3
[0045] see figure 2 As shown, on the basis of Embodiment 1, the missile also includes a start control unit 11, which is connected to the processor 1, and controls the processor 1 to sleep when the start condition does not come, and controls it when the start condition arrives. The processor 1 starts to work, and the start condition includes a predetermined time or a predetermined geographical location; in this embodiment, the start control unit 11 is a timer, and when the timer counts to a predetermined time, the The timer controls the processor 1 to start working, otherwise, the timer controls the processor 1 to sleep.
[0046] The anti-intercept missile with separation layer and smoke release function of the present invention also includes a start control unit 11, which is connected with the processor 1, and controls the processor 1 to sleep when the start condition does not come, and when the start condition When it arrives, control the processor 1 to start working. If t...
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