Electro-Mechanical Landing Gear system integration for Small Aircraft [SAT]

Topic description

Specific Challenge:

This topic aims at integration of electro-mechanical landing gear and brake system (which are being developed as part of other research projects for small aircraft) in an “aircraft zero” (iron-bird) integration and test environment, enabling its advancement from TRL3 / TRL4 to above TRL5. Please refer to the full topic descriptions document published in this call.