FIELD: weaponry.
SUBSTANCE: invention relates to rocketry, namely, to guided missile power control systems. The guided missile steering drive unit comprises steering drives, aerodynamic control surfaces and outer fairing. The latter represents a load-bearing cylindrical housing with radial holes receiving control surface axles, while every steering drive represents a separate self-contained assembly balanced relative to the drive seats arranged on the housing surface in the form of cylindrical sectors. Note that the steering drives are furnished with connector assemblies.
EFFECT: improved arrangement and operating performances, simpler design.
2 dwg
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|
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| GUIDED MISSILE AND SERVO UNIT FOR IT | 2000 |
|
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| GUIDED MISSILE | 1994 |
|
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| CONTROLLED PROJECTILE, STEERING DRIVE GROUP OF CONTROLLED PROJECTILE, PNEUMATIC DISTRIBUTION DEVICE OF STEERING DRIVE OF CONTROLLED PROJECTILE, MECHANISM OF INITIATION OF STEERING DRIVE OF CONTROLLED PROJECTILE | 2017 |
|
RU2669979C1 |
