V-22 Hardware Development Airframe
Abstract
The V-22 Hardware Development Airframe continues to fund development efforts. Continue development in support of V-22 Block upgrades, electrical system capacity efforts, Time on Wing/Reliability Improvements efforts such as testing of Additive Manufacturing processes for selected V-22 components and Safety Improvement efforts such as Cockpit Engine Health Indicator (CEHI) and gearbox vibration monitoring. Continue engineering, logistics, flight test, flight test support and address the correction of deficiencies and obsolescence. Continue V-22 software development/sustainment efforts such as transition tech demo, Modular Avionics Mission Computer Obsolescence Initiative re-design and Flight Control System. Continue V-22 integrated aircraft survivability equipment to include correcting deficiencies; radar warning system, integration with an upgraded missile warning and active infrared countermeasure system, cockpit interface units, electrical power system, rotor blade tabs, nacelle sails, Miniature Airborne Global Positioning System Receiver (MAGR2K) - which is part of DI, Defensive Weapons capabilities and providing integrated threat warning information on the aircraft main flight displays. Continue correcting deficiencies of the current EAP's and development of particle separation solutions. Continue Nacelle redesign efforts that will improve maintainability and reliability, as well as wiring redesign.
Document Details
- Document Type
- Accomplishment
- Publication Date
- Oct 01, 2020
- Source ID
- bbf43e47f34a82ce1c40e82522de2fbe
Related Documents
- Root: V-22A