Devati 191: Difference between revisions
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| Line 38: | Line 38: | ||
General characteristics | General characteristics | ||
--> | --> | ||
|crew= | |crew=1 | ||
|length m=11.1 | |length m=11.1 | ||
|length note= | |length note= | ||
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|gross weight kg=5000 | |gross weight kg=5000 | ||
|gross weight note= | |gross weight note= | ||
|max takeoff weight kg= | |max takeoff weight kg=5950 | ||
|max takeoff weight note= | |max takeoff weight note= | ||
|fuel capacity= | |fuel capacity= | ||
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|eng1 number=2 | |eng1 number=2 | ||
|eng1 name=[[ | |eng1 name=[[Devati S-P251-117 Deva]] | ||
|eng1 type=V-12 inverted liquid-cooled piston engines | |eng1 type=V-12 inverted liquid-cooled piston engines | ||
|eng1 kw=<!-- prop engines --> | |eng1 kw=<!-- prop engines --> | ||
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|eng1 kn=<!-- jet/rocket engines --> | |eng1 kn=<!-- jet/rocket engines --> | ||
|eng1 lbf=<!-- jet/rocket engines --> | |eng1 lbf=<!-- jet/rocket engines --> | ||
|eng1 note={{cvt| | |eng1 note={{cvt|1475|PS|kW hp|0}} | ||
|prop blade number=3 | |prop blade number=3 | ||
|prop name=constant-speed propellers | |prop name=light-alloy constant-speed propellers | ||
|prop dia m=<!-- propeller aircraft --> | |prop dia m=<!-- propeller aircraft --> | ||
|prop dia note= | |prop dia note= | ||
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--> | --> | ||
|max speed kmh=667 | |max speed kmh=667 | ||
|max speed note=at {{cvt| | |max speed note=at {{cvt|7000|m|0}} | ||
|cruise speed kmh= | |cruise speed kmh=445 | ||
|cruise speed note= | |cruise speed note= | ||
|stall speed kmh= | |stall speed kmh=105 | ||
|stall speed note= | |stall speed note= | ||
|never exceed speed kmh= | |never exceed speed kmh= | ||
| Line 88: | Line 88: | ||
|minimum control speed note= | |minimum control speed note= | ||
|range km= | |range km= | ||
|range note= | |range note= 2288 | ||
|combat range km= | |combat range km= 1144 | ||
|combat range note= | |combat range note= | ||
|ferry range km= | |ferry range km= 3988 | ||
|ferry range note= | |ferry range note= | ||
|endurance=<!-- if range unknown --> | |endurance=<!-- if range unknown --> | ||
|ceiling m= | |ceiling m=13000 | ||
|ceiling note= | |ceiling note= | ||
|g limits=<!-- aerobatic --> | |g limits=<!-- aerobatic --> | ||
|roll rate=<!-- aerobatic --> | |roll rate=<!-- aerobatic --> | ||
|climb rate ms= | |climb rate ms=25 | ||
|climb rate note= | |climb rate note= | ||
|time to altitude={{cvt|6000|m|0}} in 5 minutes | |time to altitude={{cvt|6000|m|0}} in 5 minutes 12 seconds | ||
|wing loading kg/m2= | |wing loading kg/m2= | ||
|wing loading note= | |wing loading note= | ||
Revision as of 20:27, 20 July 2020
| Devati 191 | |
|---|---|
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| |
| Role | Fighter Fighter-Bomber |
| National origin | Tennai |
| Manufacturer | Devati |
| First flight | 1937 |
| Introduction | 1938 |
| Retired | 1949 |
| Status | Retired |
| Primary user | Royal Tennaiite Air Force |
| Produced | 1938-1946 |
| Number built | 3,637 |
Aeroplane
Design and Development
Operational Service
Variants
Operators
Surving Aircraft
Specifications Dv 191 H5
General characteristics
- Crew: 1
- 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)
- Max takeoff weight: 5,950 kg (13,118 lb)
- Powerplant: 2 × Devati S-P251-117 Deva V-12 inverted liquid-cooled piston engines 1,475 PS (1,085 kW; 1,455 hp)
- Propellers: 3-bladed light-alloy constant-speed propellers
Performance
- Maximum speed: 667 km/h (414 mph; 360 kn) at 7,000 m (22,966 ft)
- Cruise speed: 445 km/h (277 mph; 240 kn)
- Stall speed: 105 km/h (65 mph; 57 kn)
- Combat range: 1,144 km (711 mi; 618 nmi)
- Ferry range: 3,988 km (2,478 mi; 2,153 nmi)
- Service ceiling: 13,000 m (43,000 ft)
- Rate of climb: 25 m/s (4,900 ft/min)
- Time to altitude: 6,000 m (19,685 ft) in 5 minutes 12 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