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
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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