Advanced Flight Control Actuation System (AFCAS - E/P). Fabrication and Design Verification Testing of a Dual Mode Electro/Pneumatic Actuator for the T-2C Aircraft

摘要

This is a report of the fabrication and design verification testing of a Dual Mode Electro/Pneumatic Actuator. Pneumatic mode open loop operation and control verified. Torque/Speed performance less than design goal due to excessive gear separation force.