FIELD: weapons and ammunition.
SUBSTANCE: claimed guide missile comprises the midflight stage and jettisonable booster engine. The latter is slip-coupled with midflight stage tail part by locating seat. The engine is provided with circular adapter with conical outer surface. Said adapter is fitted at the midflight stage tail ahead of the booster engine end. Said adapter is composed of spring-loaded segment inserts. The latter are fitted to be retained from opening by the booster engine front flange and by segment split ring.
EFFECT: decreased disturbances of midflight stage at separation.
2 cl, 5 dwg
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