FIELD: aviation.
SUBSTANCE: device is housed within the air vehicle frame and comprises the electrical assembly. The electrical assembly is situated transversely to the second stage outside perimeter and comprises the bottom, which is rigidly fixed in the second stage frame, where not less than two bushes with the holes for the placement of the electrical connections and the safety rope are situated. The top part of each bush is designed as the sharpened cutting edge. The safety rope one end is rigidly fixed in the bottom, and the other end and the electrical connections are rigidly connected to the clamping device, which is fixedly attached to the first stage frame. The safety rope has the smaller length than the electrical connections and is housed within the bottom front part.
EFFECT: air vehicle aerodynamic characteristics are improved, missile destruction is prevented.
2 dwg
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