Sunday, December 5, 2010

Helikopter tempur

Denel AH-2 Rooivalk

File:Denel Rooivalk flying 2006.jpg

Specifications

Data from Jane's All The World's Aircraft 2003–2004[9]

General characteristics

  • Crew: 2 (pilot & weapon systems officer)
  • Length: 18.73 m[10] (61 ft 5½ in)
  • Rotor diameter: 15.58 m (51 ft 1½ in)
  • Height: 5.19 m (17 ft 0¼ 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:Turbomeca Makila 1K2 turboshafts, 1,420 kW (1,904 shp) each
  • Internal fuel capacity: 1,854 L (489.8 US Gallons)

Performance

Armament


AgustaWestland Apache


Westland Apache AH Mk1 at a UK airshow

Specifications (Apache AH1)

Data from AgustaWestland page[32] Jane's Air Forces,[33] British Army[11]

General characteristics

  • Crew: 2
  • Length: 17.7 m (58 ft 4 in with rotors turning)
  • Rotor diameter: 14.6 m (48 ft)
  • Height: 3.87 m (12 ft 8 in)
  • Disc area: 168.11 m² (1,809.5 ft²)
  • Empty weight: 5,165 kg (11,387 lb)
  • Loaded weight: 8,006 kg (17,650 lb)
  • Max takeoff weight: 9,525 kg (21,000 lb)
  • Powerplant:Rolls-Royce/Turbomeca RTM322 turboshaft, 1,566 kW (2,100 hp) each

Performance

Armament


Eurocopter Tiger


Eurocopter Tiger HAP at the Paris Air Show 2007

Specifications (Tiger HAP)

German Tiger UHT during a looping demonstration at ILA 2006

General characteristics

  • Crew: 2 (pilot, 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 m² (1,430 ft²)
  • Empty weight: 3,060 kg (6,750 lb)
  • Max takeoff weight: 6,000 kg (13,000 lb)
  • Internal fuel capacity: 1,080 kg (2,380 lb)
  • Powerplant:MTU Turbomeca Rolls-Royce MTR390 turboshafts, 873 kW (1,170 shp) each

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)

Armament

  • Guns: ** 1× 30 mm (1.18 in) GIAT 30 cannon in chin turret

On its two inner hardpoints and two outer hardpoints the Eurocopter Tiger can carry a combination of the following weapons:

  • on each of its two inner hardpoints:
    • 2x 20 mm (0.787 in) machine cannons in a pod, or
    • 22× 68 mm (2.68 in) SNEB unguided missiles in a pod, or
    • 8x AGM-114 Hellfire laser guided missiles
  • on each of its two outer hardpoints:
    • Mistral air-to-air missiles, or
    • 12× 68 mm (2.68 in) SNEB unguided missiles in a pod

Mil Mi-28


Mil Mi-28N in flight

Specifications (Mi-28N)

Mi-28-Havoc-schema.png

Data from Jane's[16]

General characteristics

  • Crew: 1 pilot (rear), 1 navigator/weapons operator (front)
  • Length: 17.01 m (55 ft 10 in)
  • Rotor diameter: 17.20 m (56 ft 5 in)
  • Height: 4.70 m (15 ft 5 in)
  • Disc area: 232.35 m² (2,501 ft²)
  • Empty weight: 8,600 kg (18,960 lb)
  • Loaded weight: 10,700 kg (23,590 lb)
  • Max takeoff weight: 11,500 kg (25,350 lb)
  • Powerplant:Klimov TV3-117VMA turboshaft, 1,636 kW (2,194 shp) each

Performance

Armament

  • Guns: 1× chin-mounted 30 mm Shipunov 2A42 cannon with 250 rounds (±110° horizontal fire)
  • Hardpoints: Two pylons under each stub wing to mount bombs, rockets, missiles, and gun pods. Main armament configurations include:

Kamov Ka-50


Kamov Ka-50 of the Russian Air Force (VVS)

Specifications

Kamov Ka-50 Hokum graphic.gif
Kamov Ka-52 on display
Data for Ka-50, differences for Ka-52 noted.

Data from Ka-50 page,[22] Ka-52 page,[14] Donald and March[8] Aerospaceweb[23]

General characteristics

  • Crew: One (for Ka-52: two)
  • Length: 16.0 m (52 ft 6 in)
  • Rotor diameter: 14.5 m (47 ft 7 in)
  • Height: 4.93 m (16 ft 2 in)
  • Disc area: 330.3 m² (3,555 ft²)
  • Empty weight: 7,700 kg (17,000 lb)
  • Loaded weight: 9,800 kg (21,600 lb)
  • Max takeoff weight: 10,800 kg (23,810 lb)
  • Powerplant:Klimov TV3-117VK turboshafts, 1,641 kW (2,200 shp) each
  • For Ka-52:
    • Loaded weight: 10,400 kg (22,930 lb)

Performance

Armament

  • 1x mobile semi-rigid 30 mm Shipunov 2A42 cannon (460 rounds total, dual feeding AP or HE-Frag)
  • A variety of payloads on the four under-wing hardpoints, including 23 mm UPK-23-250 gun pods (240 rounds each), 2 x APU-6 Missle racks, able to accommodate a total of 12 9K121 Vikhr anti-tank missiles, Vympel R-73 (NATO: AA-11 Archer) air-to-air missiles, 80 x 80 mm S-8 rockets and 20 x 122 mm S-13 rocket, Kh-25 semi-active laser guided tactical air-to-ground missiles, presumably S-25/S-25L high caliber rockets, 4x 250 kg (550 lb) bombs or 2x 500 kg (1,100 lb) bombs, 500 L (130 US gal) external fuel tanks. Reportedly, twin Igla light air-to-air missile launchers under each wingtip countermeasure pod (total 4 missiles). Maximum total payload 2,000 kg.[17]
  • Two pods on the wingtips with flare and chaff countermeasure dispensers, 4 UV-26 dispensers each (total 512 chaff/flare cartridges in each pod)




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