![]() The HTAS maximizes commonality in design for both the elevator and rudder control. The main rotor servoactuators leverage Parker’s experience on the SB>1 DEFIANT® and S-97 RAIDER® demonstrators. Ballistic tolerance for the product comes from legacy experience on the UH-60 Black Hawk® and AH-64 Apache®. The MRS reflect Parker Aerospace’s investment and experience in fly-by-wire technology with an optimized design that saves weight and improves reliability in a harsh helicopter environment. The FCMs facilitate reduced installation and maintenance times.įlight controls with the lowest risk and weight, and highest reliability These modules enable very condensed, lighter-weight packaging and eliminate the interconnecting tubing/hoses and associated leakage concerns. The highly integrated hydraulic flight control modules (FCM) include the reservoir, filtration, valves and sensors. These benefits provide lower life cycle costs for the U.S. ![]() ![]() The next-generation design offers significant efficiency benefits such as lighter weight and less heat rejection, resulting in reduced fuel burn compared to alternative pumps. ![]() The suite utilizes features that Parker Aerospace has developed in its next-generation pump independent research and development program, as well as lessons learned from extensive experience with 5,000 psi commercial products. ![]() The hydraulic pump suite for the DEFIANT X® aircraft will consist of main gearbox pumps and a smaller auxiliary pump. ![]()
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