UFAG 60.03: Difference between revisions
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The '''UFAG 60.03''', prototype for proposed production as the '''UFAG C.II''', was a reconnaissance aircraft of the Austro-Hungarian air forces (''Luftstreitskrafte''), in the [[First World War]].<ref name=Grosz>{{cite book |last= Grosz |first= Peter M. |title=Austro-Hungarian Army Aircraft of World War One |year=2002 |publisher=Flying Machine Press |location= Colorado |pages=265–267 }}</ref> The C.II fared well in the 1918 C-class trials and |
The '''UFAG 60.03''', prototype for proposed production as the '''UFAG C.II''', was a reconnaissance aircraft of the Austro-Hungarian air forces (''Luftstreitskrafte''), in the [[First World War]].<ref name=Grosz>{{cite book |last= Grosz |first= Peter M. |title=Austro-Hungarian Army Aircraft of World War One |year=2002 |publisher=Flying Machine Press |location= Colorado |pages=265–267 }}</ref> The C.II fared well in the 1918 C-class trials and production was planned but abandoned with the [[armistice]] in November 1918. The sole UFAG 60.03 was offered for sale to the Czecho-Slovakian government in 1920.<ref name=Grosz/> |
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Revision as of 15:33, 14 September 2019
| C.II / 60.03 | |
|---|---|
| Role | Reconnaissance aircraft |
| National origin | Austro-Hunagarian Empire |
| Manufacturer | UFAG |
| Designer | Béla Oravecz |
| First flight | july or August 1918 |
| Number built | 1 |
| Developed from | Brandenburg C.I(U) |
The UFAG 60.03, prototype for proposed production as the UFAG C.II, was a reconnaissance aircraft of the Austro-Hungarian air forces (Luftstreitskrafte), in the First World War.[1] The C.II fared well in the 1918 C-class trials and production was planned but abandoned with the armistice in November 1918. The sole UFAG 60.03 was offered for sale to the Czecho-Slovakian government in 1920.[1]
Specifications (60.03)
Data from Austro-Hungarian Army Aircraft of World War One[1]
General characteristics
- Crew: 2
- Upper wingspan: 10.3 m (33 ft 10 in)
- Lower wingspan: 9.74 m (31 ft 11 in)
- Wing area: 28.64 m2 (308.3 sq ft)
- Empty weight: 750 kg (1,653 lb)
- Gross weight: 1,150 kg (2,535 lb)
- Powerplant: 1 × Hiero 6 6-cylinder water-cooled in-line piston engine, 170 kW (230 hp)
- Propellers: 2-bladed wooden fixed-pitch propeller
Performance
- Time to altitude:
- 1,000 m (3,281 ft) in 4 minutes 45 seconds
- 2,000 m (6,562 ft) in 10 minutes 53 seconds
- 3,000 m (9,843 ft) in 20 minutes 46 seconds
- 4,000 m (13,123 ft) in 31 minutes 14 seconds
Armament
- provision for fixed and flexibly mounted guns as well as light bombs