Devati 191: Difference between revisions
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|guns=<br/> | |guns=<br/> | ||
:* 4 × {{cvt|7.92|mm|3}} [[ | :* 4 × {{cvt|7.92|mm|3}} [[Basu HV 80]] machine guns in fuselage sides | ||
:* 2 × {{cvt|20|mm|3}} [[ | :* 2 × {{cvt|20|mm|3}} [[Basu FG 20-20 cannon]] in lower fuselage | ||
* 4× M10 three-tube 4.5 in (112 mm) [[M8 (rocket)|M8 rocket]] launchers; '''or''': | |||
** Inner hardpoints: | |||
*** 2× {{convert|2000|lb|kg|0|abbr=on}} bombs or drop tanks; '''or''' | |||
*** 2× {{convert|1000|lb|kg|0|abbr=on}} bombs or drop tanks, plus either | |||
**** 4× {{convert|500|lb|kg|0|abbr=on}} bombs or | |||
**** 4× {{convert|250|lb|kg|0|abbr=on}} bombs; '''or''' | |||
*** 6× {{convert|500|lb|kg|0|abbr=on}} bombs; '''or''' | |||
*** 6× {{convert|250|lb|kg|0|abbr=on}} bombs | |||
** Outer hardpoints: | |||
*** 10× 5 in (127 mm) [[HVAR]]s (High Velocity Aircraft Rockets); '''or''' | |||
*** 2× {{convert|500|lb|kg|0|abbr=on}} bombs; '''or''' | |||
*** 2× {{convert|250|lb|kg|0|abbr=on}} bombs | |||
}} | }} | ||
Revision as of 20:32, 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) Basu HV 80 machine guns in fuselage sides
- 2 × 20 mm (0.787 in) Basu FG 20-20 cannon in lower fuselage
- 4× M10 three-tube 4.5 in (112 mm) M8 rocket launchers; or:
- Inner hardpoints:
- 2× 2,000 lb (907 kg) bombs or drop tanks; or
- 2× 1,000 lb (454 kg) bombs or drop tanks, plus either
- 4× 500 lb (227 kg) bombs or
- 4× 250 lb (113 kg) bombs; or
- 6× 500 lb (227 kg) bombs; or
- 6× 250 lb (113 kg) bombs
- Outer hardpoints:
- 10× 5 in (127 mm) HVARs (High Velocity Aircraft Rockets); or
- 2× 500 lb (227 kg) bombs; or
- 2× 250 lb (113 kg) bombs
- Inner hardpoints: