FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and may be used for release of space equipment release. Proposed release comprises perforated heat conducting cylindrical case, cover, linearly moving element composed of spring-loaded piston, retainer composed of two thermoplastic inserts, spring, guide, moving element, moving element tooth and cotter-pin linearly displacing along aforesaid guide. Said spring and thermoplastic insert are separated by a cap, while moving element travel exceeds the guide size.
EFFECT: alternative principle of operation in space.
2 cl, 3 dwg
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