Do228 – DLR Multi role turboprop twin engine test aircraft

Flugversuchsträger des DLR : DO 228

Validation of innovative Air Traffic Management systems by flight testing of new sensors or equipment.

Performance Data:
Max. cruising speed:  160 kt
Max. speed:  200 kt depending on equipment
MTOW:  5980 kg
Max. altitude:  25000 ft
Endurance:  approximately 9 hours
Max. range:   1320 nautical miles (2445 km; 1519 miles)

For test equipment the power supplies are 28V, 115V/400 Hz and 220V/50 Hz

Basic equipment:
• Inertial Navigation System LTN 90
• VOR and ILS receivers
• Personal Computers for data logging or data display
• Omnistar system with Novatel GPS receiver as reference for positioning. Decimetre accu-racy will be achieved.
• Antennas can be mounted in two positions (aft of cockpit and rear) on the upper side and in the back on aircraft underside.
• Versatile Racks for test systems are provided which can contain equipment of up to 200 kg.
• Various hardpoints and hatches for cameras and sensors are also available.