FIELD: rocket technology.
SUBSTANCE: invention relates to rocket technology, namely to a detachable braking and stabilization system of a warhead of an unmanned aerial vehicle. An attachment and separation unit of the braking and stabilization system of the warhead of the unmanned aerial vehicle contains a case, to which the braking and stabilization system is rigidly attached, as well as a pyrotechnic mechanism consisting of a powder charge and a squib. The case of the unit is attached to a case of the warhead due to an annular groove on the case of the warhead, in which two half-rings are installed, which have the possibility of reclining in the radial direction, and which are interconnected by explosive bolts. Half-rings are attached to the case by means of rods connected to pistons installed in a collector with the pyrotechnic mechanism and having the possibility of lifting rods with half-rings. The collector with the pyrotechnic mechanism is installed in the case of the attachment unit.
EFFECT: reduction in the impact of axial overloads on the warhead when the braking and stabilization system of the warhead of the unmanned aerial vehicle is separated.
1 cl, 3 dwg
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Authors
Dates
2022-07-04—Published
2020-09-07—Filed