发明名称 |
GUIDED MISSILE LAUNCHING DEVICE |
摘要 |
FIELD: guided missile launching devices. SUBSTANCE: launching device is made as a pack, whose base chamber accommodates the projectile tail with pressure source and aerodynamic surfaces. The pressure source is made in the form of containers with solid propellant charges and igniter squibs. Each pressure container has a pair of nozzles located perpendicularly to the projectile longitudinal axis and directed opposite each other. The containers are furnished with controllable valves, and the pack - with a lock for retention of projectile. EFFECT: storage and transportation of projectile and control of it in the flight launching phase. 5 cl, 5 dwgp
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申请公布号 |
RU2114371(C1) |
申请公布日期 |
1998.06.27 |
申请号 |
RU19970112945 |
申请日期 |
1997.07.28 |
申请人 |
GOSUDARSTVENNOE MASHINOSTROITEL'NOE KONSTRUKTORSKO;G MASHINOSTROITEL NOE K |
发明人 |
VATOLIN V.V.;DUL'KIN I.I.;ELETSKIJ V.K.;LAZHENITSYN I.A.;LEVISHCHEV O.N.;MOS'KIN A.M.;SVISHCHEV V.I.;SOKOLOVSKIJ G.A. |
分类号 |
F41F3/042;F42B12/00;(IPC1-7):F41F3/042 |
主分类号 |
F41F3/042 |
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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