| 摘要 |
The present invention comprises a control surface actuation system capable of disposition within a restricted volume. The present actuation system and control surface is disposed outboard of the missile due to space limitations imposed by an unusually large nozzle diameter. The system comprises four independent electro-hydraulic actuators of the push-push configuration for driving four aerodynamic control surfaces arranged in cruciform and disposed at the aft end of the missile. The actuation system arrangement allows passage of the missile through existing launchers having typical volume restraints.
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