NASA-LLIS-2839
Lessons Learned – Reduced Torque Output from Electro-Mechanical Actuators
| Organization: | NASA |
| Publication Date: | 4 May 2010 |
| Status: | active |
| Page Count: | 2 |
scope:
Abstract:
Reduced torque output of the orbiter's electromechanical actuators has been a problem for the Shuttle Program. It has resulted in unplanned work to test, remove, and refurbish the actuators. Disassembly and inspection has revealed that the torque reduction is a result of problems with the torque limiters and the motor clutch/brake assemblies in the actuators. Refurbishment is a lengthy process because of the difficulty involved in setting the torque limiter to operate through the required temperature range. The next generation of actuators should have a better design, or the mechanical system should be capable of withstanding the maximum output loads of the actuator.
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