Devati 191

Devati 191
Role	Fighter Fighter-Bomber Aerial Reconnassance
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

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)
• Range: 2,288 km (1,422 mi; 1,235 nmi)
• 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) Hornet 7 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