FIELD: rocketry.
SUBSTANCE: invention is used in rocket engineering for actuation of electric ignition devices of launching and onboard systems of rocket projectiles. Disclosed is a magnetoelectric pulse generator, which consists of permanent magnets 1 and 2, upper 3 and lower 4 yokes, between which there is electromagnetic coil 5. Inside coil 5 anchor 6 is placed, which lies on stops 7 and 8 of upper 3 and lower 4 yokes, respectively. One end of armature 6 interacts with spring mechanism, which passes through holes of upper 3 and lower 4 yokes and consists of metal cup 9 and two springs: external 10 and internal 11.
EFFECT: reducing the size and weight of the magnetoelectric pulse generator, as well as simplifying its design and increasing the power of the generated electric pulse.
1 cl, 1 dwg
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