发明名称 ROCKET PROJECTILE FASTENING DEVICE
摘要 FIELD: defensive equipment, applicable for fastening of small-sized rocket projectiles with a solid-propellant rocket engine in tubular transport-launching packs. SUBSTANCE: fastening device is made in the form of a holder consisting of two pairs of half-rings. The inner half-rings are installed in a groove made on the booster engine case. The outer half-rings are installed in a groove made on the external surface of the inner half-rings and engageable with a trapeziform groove made on the inner surface of the pack tube. Rocket projectile is locked in the pack due to installation of locking L-shaped plates in the joint of the outer half-rings, having a leg located opposite the projectile engine exit nozzle. EFFECT: enhanced accuracy of fire due to reduced disturbances acting on projectile at launching. 2 cl, 4 dwgl
申请公布号 RU2107247(C1) 申请公布日期 1998.03.20
申请号 RU19960123081 申请日期 1996.12.05
申请人 KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA 发明人 SHIPUNOV A.G.;TIKHONOV V.P.;ZAKHAROV L.G.;KOPYLOV JU.D.;PARFENOV P.P.;SHIPUNOV A.G.;TIKHONOV V.P.;ZAKHAROV L.G.;KOPYLOV JU.D.;PARFENOV P.P.
分类号 F41F3/04;(IPC1-7):F41F3/04 主分类号 F41F3/04
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