Fichas tecnicas de helicpteros (2 tripulantes)

Bell AH-1 Cobra

General characteristics

Crew: 2: one pilot, one co-pilot/gunner (CPG) Length: 53 ft (16.2 m) (with both rotors turning) Rotor diameter: 44 ft (13.4 m) Height: 13 ft 6 in (4.12 m) Empty weight: 5,810 lb (2,630 kg) Max. takeoff weight: 9,500 lb (4,310 kg) Powerplant: 1 Lycoming T53-L-13 turboshaft, 1,100 shp (820 kW) Rotor system: 2 blades on main rotor, 2 blades on tail rotor Fuselage length: 44 ft 5 in (13.5 m) Stub wing span: 10 ft 4 in (3.15 m)

Performance

Never exceed speed: 190 knots (219 mph, 352 km/h) Maximum speed: 149 knots (171 mph, 227 km/h) Range: 310 nmi (357 mi, 574 km) Service ceiling: 11,400 ft (3,475 m) Rate of climb: 1,230 ft/min (6.25 m/s)

Aerospatlale Sud-Ouest Djinn

General characteristics

Crew: Two Length: 5.30 m (17 ft 4 in) Main rotor diameter: 11 m (36 ft 1 in) Height: 2.6 m (8 ft 6 in) Main rotor area: 95.03 m2 (1022.96 ft2) Empty weight: 360 kg (704 lb) Gross weight: 800 kg (1,764 lb) Powerplant: 1 Turbomeca Palouste IV turbo-compressor, 179 kW (240 hp)

Performance

Maximum speed: 130 km/h (81 mph) Range: 220 km (137 miles) Endurance: 2 hours 15 min Service ceiling: 3,000 m (9,842 ft)

Boeing AH-64 Apache

General characteristics

Crew: 2 (pilot, and co-pilot/gunner) Length: 58.17 ft (17.73 m) (with both rotors turning) Rotor diameter: 48 ft 0 in (14.63 m) Height: 12.7 ft (3.87 m) Disc area: 1,809.5 ft (168.11 m) Empty weight: 11,387 lb (5,165 kg) Loaded weight: 17,650 lb (8,000 kg) Max. takeoff weight: 23,000 lb (10,433 kg) Powerplant: 2 General Electric T700-GE-701 and later upgraded to T700-GE701C (1990present) & T700-GE-701D (AH-64E) turboshafts, -701: 1,690 shp, 701C: 1,890 shp, 701D: 2,000 shp (-701: 1,260 kW, 701C: 1,490 kW, 701D: 1,490 kW) each Fuselage length: 49 ft 5 in (15.06 m) Rotor systems: 4 blade main rotor, 4 blade tail rotor in non-orthogonal alignment

Performance

Never exceed speed: 197 knots (227 mph, 365 km/h) Maximum speed: 158 knots (182 mph, 293 km/h) Cruise speed: 143 knots (165 mph, 265 km/h) Range: 257 nmi (295 mi, 476 km) with Longbow radar mast Combat radius: 260 nmi (300 mi, 480 km) Ferry range: 1,024 nmi (1,180 mi, 1,900 km) Service ceiling: 21,000 ft (6,400 m) minimum loaded Rate of climb: 2,500 ft/min (12.7 m/s) Disc loading: 9.80 lb/ft (47.9 kg/m) Power/mass: 0.18 hp/lb (0.31 kW/kg)

Cicar CH-14

General characteristics

Crew: 2 Length: 11.8 m (38 ft 7 in) Rotor diameter: 10.00 m (32 ft 8 in) Height: 3.3 m (11 ft 0 in) Empty weight: 750 kg (1650 lb) Max. takeoff weight: 1,450 kg (3,190 lb) Powerplant: 1 Rolls-Royce Allison 250-C20-B turboshaft, 313 kW (420 shp) Propellers: two blade rotor

Performance

Maximum speed: 240 km/h (149 knots, mph) Cruise speed: 210 km/h (131 knots, mph) Range: 510 km (275 nm, 320 mi) Ferry range: 1,000 km (540 nm, 620 mi) Service ceiling: 4,500 m (14,764 ft) Rate of climb: 8 m/s (1,925 ft/min)

Denel Rooivalk

General characteristics

Crew: 2 (pilot & weapon systems officer) Length: 18.73 m[14] (61 ft 5 12 in) Rotor diameter: 15.58 m (51 ft 1 12 in) Height: 5.19 m (17 ft 0 in) Disc area: 190.60 m2 (2,052.1 sq ft) Empty weight: 5,730 kg (12,632 lb) Loaded weight: 7,500 kg (16,535 lb) Max. takeoff weight: 8,750 kg (19,290 lb) Powerplant: 2 Turbomeca Makila 1K2 turboshafts, 1,420 kW (1,904 shp) each Internal fuel capacity: 1,854 L (489.8 US gallons)

Performance

Never exceed speed: 309 km/h (167 knots, 193 mph) Cruise speed: 278 km/h (150 knots, 173 mph) at sea level (max cruise) Range: 740 km (380 nmi, 437 mi) at sea level(max internal fuel) Ferry range: 1,335 km (720 nmi, 829 mi) at 1525 m (5,000 ft) (max external fuel) Service ceiling: 6,100 m (20,000 ft) Rate of climb: 13.3 m/s (2,620 ft/min)

Armament

1 F2 20 mm cannon, 700 rounds 8 or 16 Mokopa ZT-6 long-range anti-tank guided missiles (ATGM), 4 MBDA Mistral air-to-air missiles, 38 or 76 70 mm folding fin aerial rockets (FFAR)

Eurocopter Tiger

General characteristics

Crew: Two: pilot and weapon systems officer Length: 14.08 m fuselage (46 ft 2 in) Rotor diameter: 13.00 m (42 ft 8 in) Height: 3.83 m (12 ft 7 in) Disc area: 133 m (1,430 ft) Empty weight: 3,060 kg (6,750 lb) Max. takeoff weight: 6,000 kg (13,000 lb)) Powerplant: 2 MTU Turbomeca Rolls-Royce MTR390 turboshafts, 958 kW (1.303 shp) each Internal fuel capacity: 1,080 kg (2,380 lb)

Performance

Maximum speed: 290 km/h with mast, 315 km/h without mast (157 knots, 181 mph with mast, 170 knots or 196 mph without mast) Range: 800 km (430 nm, 500 mi) combat (with external tanks in the inboard stations: 1,300km) Service ceiling: 4,000 m (13,000 ft) Rate of climb: 10.7 m/s (2,105 ft/min)

Kawasaki OH-1

General characteristics

Crew: 2, pilot and observer Length: 12 m (39 ft 4 in) Height: 3.8 m (12 ft 6 in) Empty weight: 2,450 kg (5,401 lb) Max takeoff weight: 4,000 kg (8,818 lb) Powerplant: 2 Mitsubishi TS1-M-10 turboshaft engines, 660 kW (890 hp) each Main rotor diameter: 11.6 m (38 ft 1 in) Main rotor area: 105.7 m2 (1,138 sq ft)

Performance

Maximum speed: 278 km/h (173 mph; 150 kn) Cruising speed: 220 km/h (137 mph; 119 kn) Range: 540 km (336 mi; 292 nmi) Service ceiling: 4,880 m (16,010 ft)

Lockheed AH-56 Cheyenne

General characteristics

Crew: Two; one pilot, one copilot/gunner (front seat) Length: 54 ft 8 in (16.66 m) Rotor diameter: 51 ft 3 in (15.62 m) Height: 13 ft 8.5 in (4.18 m) Empty weight: 12,215 lb (5,540 kg) Loaded weight: 18,300 lb (8,300 kg) Max. takeoff weight: 25,880 lb (11,740 kg) Powerplant: 1 General Electric T64-GE-16 turboshaft, 3,925 shp (2,930 kW) Rotor systems: 4 blades on main rotor, 4 blades on tail rotor, 3 blades on pusher propeller

Performance

Maximum speed: 212 knots (244 mph, 393 km/h) Cruise speed: 195 knots (225 mph, 362 km/h) Range: 1,063 nmi (1,225 mi, 1,971 km) Service ceiling: 20,000 ft (6,100 m) Rate of climb: 3,000 ft/min (15.23 m/s)

Boeing-Sikorsky RAH-66 Comanche

General characteristics

Crew: 2 Length: 46.85 ft (14.28 m) Rotor diameter: 39.04 ft (11.90 m) Height: 11.06 ft (3.37 m) Disc area: 1,197 ft (111 m) Empty weight: 9,300 lb (4,218 kg) Loaded weight: 12,349 lb (5,601 kg) Useful load: 5,062 lb (2,296 kg) Max. takeoff weight: 17,408 lb (7,896 kg) Powerplant: 2 LHTEC T800-LHT-801 turboshaft, 1,563 hp (1,165 kW) each Fuselage length: 43.31 ft (13.20 m) Rotor systems: 5-bladed main rotor, 8-bladed fan-in-fin anti-torque system (FANTAIL)

Performance

Maximum speed: 175 knots (201 mph, 324 km/h) Cruise speed: 165 knots (190 mph, 306 km/h) Range: 262 nmi (302 mi, 485 km) on internal fuel Combat radius: 150 nmi (173 mi, 278 km) on internal fuel Ferry range: 1,200 nmi (1,380 mi, 2,220 km) Endurance: 2.5 hr Service ceiling: 14,980 ft (4,566 m) Rate of climb: 895 ft/min (4.55 m/s)