High efficiency full electrical low pressure Compartment Pressure Control System for tilt-rotor applications

Topic description

Specific Challenge:

The purpose activity requires the development, testing and qualification of a full electrical modular-based Low Pressure Compartment Pressure Control System, including analysis to determine the best architecture taking into account the special flight characteristics of a Tilt Rotor and an occupants range from 9 to 30. Please refer to the full topic descriptions document published in this call.