Devati 191: Difference between revisions

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

Revision as of 20:33, 20 July 2020

Aeroplane

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

@@ Line 112: / Line 112: @@
 :* 4 × {{cvt|7.92|mm|3}} [[Basu HV 80]] machine guns in fuselage sides
 :* 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''':
+* 4× M10 three-tube 4.5 in (112 mm) [[Hornet 7 (rocket)|Hornet 7 rocket]] launchers; '''or''':
 ** Inner hardpoints:
 *** 2× {{convert|2000|lb|kg|0|abbr=on}} bombs or drop tanks; '''or'''