发明名称 |
GUIDED MISSILE ACTUATOR ASSEMBLY |
摘要 |
FIELD: defence equipment, applicable in design development of guided missiles. SUBSTANCE: actuator assembly improves the dynamic characteristics of the actuator assembly by increasing the developed torque due to spacing of the hinge axes of each pair of control surfaces along the missile longitudinal axis at a distance of not more than 0.4 of the caliber of the control actuator compartment, arrangement of the actuators on different sides of the control - surface hinge axes. EFFECT: improved dynamic characteristics. 2 dwgh
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申请公布号 |
RU2101667(C1) |
申请公布日期 |
1998.01.10 |
申请号 |
RU19960119611 |
申请日期 |
1996.10.01 |
申请人 |
KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA |
发明人 |
ZYBIN I.M.;FIMUSHKIN V.S.;GOLOVANOV N.S.;ZYBIN I.M.;FIMUSHKIN V.S.;GOLOVANOV N.S. |
分类号 |
F42B15/00;F42B10/60;(IPC1-7):F42B15/00 |
主分类号 |
F42B15/00 |
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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