UNLIMITED FREE
ACCESS
TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

NASA-LLIS-2839

Lessons Learned – Reduced Torque Output from Electro-Mechanical Actuators

active, Most Current
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.

Document History

NASA-LLIS-2839
May 4, 2010
Lessons Learned – Reduced Torque Output from Electro-Mechanical Actuators
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...
Advertisement