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Specialty & Custom
1994: Rocket Nozzle Control
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Foreword
2003
Direct Drives (ALMA)
2001
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2000
Multiple Spindle Drives
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1995
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1994
Rocket Nozzle Control
1992
Large Drives (VLT)

High performance electric linear actuators

Ultra light electrical linear actuators find a novel application in nozzle attitude control for rocket engines of space vehicles.
The linear actuator, controlled by the inertial guidance system of the missile, varies the attitude of the nozzle with respect to missile axis thus holding the course and the vehicle stability against air turbulence during the atmospheric path.
 
The electric linear actuators replace the more traditional hydraulic servo actuators, resulting in a faster response, higher bandwidth system.
Additional advantages are a lower mass and a simpler machanical system. The use of electronic linear actuators improves the launch reliability with strong atmospheric turbulence.
The electronic linear actuator developed by Phase Motion Control for the Scout booster is capable of 26000 N thrust, 5 m/s speed within a total mass of just 6.6 Kg.
 


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