FIELD: devices for separation of flying vehicle structural members; space engineering; aeronautical engineering. SUBSTANCE: proposed device has housing with inner cavity whose bottom is made in form of hemisphere, explosive charge chamber, diaphragm and rod. Diaphragm has hole for connection of above-diaphragm cavity with end surface of rod. Rod is mounted for motion relative to diaphragm. EFFECT: possibility of performing considerable motion of rod without increase of diameter of diaphragm. 2 dg
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Authors
Dates
2004-02-27—Published
2001-07-02—Filed