DA 100 EFI MIL SPEC UAV Engine comes fitted with state of the art electronic fuel injection. This mil spec version provides a fuel injection system that has been in service on over 700 aircraft and has more than 67,000 flight hours in various environments around the world. The system has been tested to 20,000 ft altitude and temperatures ranging from -10°F to 120°F.
This system followed the test methods under MIL-STD-810, testing out the majority of the laboratory methods available.
This 3 phrase brushless alternator is direct driven on the engine crankshaft. The stator is mounted to the crankshaft casing, with the rotor spinning on the crankshaft.
The system includes a 500 W Power Management Unit with an integrated starter controller, allowing the engine to start remotely. The PMU provides three lines with a chosen voltage in the range: 24 – 28 VDC at 12.5A or 350W max, 12 – 15 VDC at 9A or 108W, and 4.8 – 8 VDC at 8A or 42W.
Configurable with LiIon, LiPo, LifePO4, SLA, NiCad, NiMH, and Lead Acid Battery.
Lead Time -
8 – 10 weeks
Weight (engine with intake) -
2.5 kg, 5.57 lb
Weight (ECU) -
70 g, 0.15 lb
Weight (Fuel Pump box) -
400 g, 0.88 lb
Standard Operating Speed -
1,200 to 6,800 RPM
Voltage -
10 V to 15 V
Power Draw -
1 Amp peak, 1 hour/1,000 mAh