AEG D.I
The AEG DI was a biplane, which was developed in 1917. The aircraft was a single-seat fighter, but of which only three prototypes were made , but were not very successful and had recorded several crashes. After these setbacks, the pattern was not developed further.
The second prototype is often referred to as the AEG D-II, the third as AEG D.III.
Building on the basic concept of the DI was developed at AEG a triple-deck version, which is also not successful Dr.I.
Specifications
- Overall length: 6.1 m
- Height: 2.65 m
- Wingspan: 8.5 m
- Wing area: 16.14 m²
- Maximum takeoff weight: 940 kg
- Empty weight: 685 kg
- Maximum speed: 205 km / h
BI | B. II | B. III | CI | C.II | C. III | C.IV | C.IV.N | CV | C.VI | C.VII | C.VIII | C.VIII Dr | DI | D.II | D.III | DJ.I | Dr.I | FI | GI | G.II | G.III | G.IV | GV | JI | J.II | PE | RI
Plant names: Z.1 | Z.2 | Z.3 | Z.6 | line 9
Other: AEG helicopter | Wagner Owl
- AEG (airplane)
- Military Aircraft
- D- type aircraft of the German Air Force in World War I
- Single Engine aircraft