AEG Dr.I

The AEG Dr.I was a single-seat fighter aircraft manufactured by the department of aircraft of the General Electric Company. It was a triple-deck version of the AEG DI, which was developed in 1917. However, the flight behavior of the machine was not satisfied, so that only one prototype was built.

Specifications

  • Length: 6.1 m
  • Wingspan: 9.4 m
  • Empty weight: 710 kg
  • Maximum takeoff weight: 970 kg
  • Maximum speed: 170 km / h
  • Powerplant: 1 x liquid cooled Mercedes D IIIa inline six-cylinder engine with 160 hp
  • Armament: 2 x MG 08 /15
Triplane AEG D.I AEG B.I AEG B.II AEG B.III AEG C.I AEG C.II AEG C.III AEG C.IV AEG C.V AEG C.VII AEG C.VIII AEG DJ.I AEG J.I AEG J.II AEG R.I
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