| Technical data | |
|---|---|
| Type | Meller-I |
| Year | 1913 |
| Crew | 1 |
| Engines | 1*80hp Salmson |
| Length | 8.1m |
| Wingspan | 13.7m |
| Wing area | 35.0m2 |
| Empty weight | 460kg |
| Loaded weight | 710kg |
| Wing Load (kg/m2) | 20.3 |
| Power load (kg/hp) | 7.1 |
Meller-III, Dux
|
Differed from Nieuport-IV by strengthened undercarriage, added ailerons and tail (from Farman-XVI). Instead of single Nieuport propeller, two tractor propellers were installed on the wing, driven by chains. Performance was quite poor.
No production.
References:
- "History of aircraft construction in the USSR", Vol.1 p.105-106;
