Devati 191: Difference between revisions
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Revision as of 18:27, 20 July 2020
| Devati 191 | |
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| Role | Heavy Fighter |
| National origin | Tennai |
| Manufacturer | Devati |
| First flight | 1937 |
| Introduction | 1938 |
| Retired | 1946 |
| Status | Retired |
| Primary user | Royal Tennaiite Air Force |
| Produced | 1938-1944 |
| Number built | 3,637 |
Aeroplane
Design and Development
Operational Service
Variants
Operators
Surving Aircraft
Specifications Dv 191 H5
General characteristics
- Crew: 2
- Length: 11.1 m (36 ft 5 in)
- Wingspan: 15.3 m (50 ft 2 in)
- Height: 3.85 m (12 ft 8 in)
- Wing area: 30.4 m2 (327 sq ft)
- Empty weight: 3,600 kg (7,937 lb)
- Gross weight: 5,000 kg (11,023 lb)
- Powerplant: 2 × Junkers Jumo 210Ga V-12 inverted liquid-cooled piston engines 680 PS (500 kW; 671 hp)
- Propellers: 3-bladed constant-speed propellers
Performance
- Maximum speed: 667 km/h (414 mph; 360 kn) at 4,000 m (13,123 ft)
- Service ceiling: 10,000 m (33,000 ft)
- Time to altitude: 6,000 m (19,685 ft) in 5 minutes 48 seconds
Armament
- Guns:
- 4 × 7.92 mm (0.312 in) MG 17 machine guns in fuselage sides
- 2 × 20 mm (0.787 in) MG FF cannon in lower fuselage