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Application
Missile and launch vehicles
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FEATURES
High-temperature applications for harsh environments • High shock and G-load capability
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Stroke Range
±3 - ±45 degrees
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Shelf Life (Months)
120 - 180
Our missile control actuation systems (CAS) include control electronics which provide electrical power and closed loop feedback control to the DC motors, converting electrical energy to rotary motion. The control electronics receive aerosurface position commands from the missiles guidance section through either an analog or digital communication interface. Rotary- or linear-output motion may be accommodated through a series of mechanical gear reduction stages connecting the DC motor and the aerosurface.