Devati 191

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Devati 191
Focke-Wulf Fw 187 (15083509087).jpg
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

Design and Development

Operational Service

Variants

Operators

Surving Aircraft

Specifications Dv 191 H5

Devati 191 orthograhic.jpg

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× 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