Описание
Страна: Австро-Венгрия
Год: 1917
Fighter
Варианты
- Lohner - 10.20 Spuckerl / Type AA - 1916 - Австро-Венгрия
- Lohner - Dr.I / Type A - 1917 - Австро-Венгрия
- W.Green, G.Swanborough The Complete Book of Fighters
- P.Grosz, G.Haddow, P.Shiemer Austro-Hungarian Army Aircraft of World War One (Flying Machines)
- E.Hauke, W.Schroeder, B.Totschinger Die Flugzeuge der k.u.k. Luftfahrtruppe und Seeflieger 1914-1918
-
-
P.Grosz, G.Haddow, P.Shiemer - Austro-Hungarian Army Aircraft of World War One /Flying Machines/
The Lohner Dr.I 111.04 (Type A) prototype, completed in June 1917, was one of the first fighter triplanes built by a Central Power.
Tested in 1917, the Typ A triplane was destined to be the last of the Lohner fighters. -
P.Grosz, G.Haddow, P.Shiemer - Austro-Hungarian Army Aircraft of World War One /Flying Machines/
This view of the Lohner Dr.I 111.04 shows the slanted wing strut configuration, the reasons for which are not readily apparent. Only one Lohner Dr.I prototype was built. The workmanship and finish were good, but the design itself was not satisfactory. The Dr.I was slightly faster and had a better climb rate than the Lohner D.I biplane with the same engine, which was unusual for a triplane development of an earlier biplane design. Regardless, poor flying qualities doomed the design.
-
-
W.Green, G.Swanborough - The Complete Book of Fighters
The Lohner Typ A (111.04) fighter triplane.
-
W.Green, G.Swanborough The Complete Book of Fighters
LOHNER TYP A (111.04) Austria-Hungary
Possessing fundamentally similar fuselage and tail surfaces to the final Typ AA biplane, the Typ A (111.04) triplane was completed on 23 June 1917. Similarly powered and armed to the preceding Lohner fighters, the Typ A had comparatively high aspect ratio wings braced by a unique canted strut arrangement. Official trials were conducted on 7 July 1917 with mediocre results, and the prototype was returned to the Lohnerwerke for modification. It reappeared in September 1917, and subsequent performance trials proved satisfactory, but the handling characteristics were poor and view from the cockpit was deemed inadequate, with the result that the programme was terminated.
Max speed, 111 mph (178 km/h).
Time to 3,280 ft (1 000 m), 2.8 min.
Range, 221 mis (356 km).
Empty weight, 1,527 lb (692,5 kg).
Loaded weight, 2,041 lb (926 kg).
Span, 28 ft 10 1/2 in (8,80 m).
Length, 20 ft 10 in (6,35 m).
Height, 9 ft 10 1/8 in (3,00 m).
Wing area, 226.05 sqft (21,00 m2).
Описание:
