데넬 AH-2A 루이발크

데넬 루이발크

국가남아프리카 공화국
형식공격 헬리콥터
첫 비행1990년 2월 11일
내장12

Denel Rooivalk (이전에 AH-2 및 CSH-2로 지정됨)는 남아프리카의 Denel Aviation에서 제조 한 공격 헬리콥터입니다. 루이발크(Rooivalk)는 아프리칸스어로 "붉은 팔콘(Red Falcon)"을 뜻하며, 이는 황조롱이를 의미합니다. 이 유형의 개발은 Atlas Aircraft Corporation에 의해 1984 년에 시작되었으며, 개발은 Atlas Oryx 수송 헬리콥터와 밀접하게 연결되어 있으며, 두 항공기 모두 Aérospatiale SA 330 Puma를 기반으로하며 동시에 개발을 시작했습니다.

소스: 데넬 루이발크 ― 위키

데넬 AH-2A 루이발크
사진 작가Unknow
로컬라이제이션Unknow
사진64
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공격 헬리콥터 - 아마존


General Characteristics (Rooivalk Mk 1F)

The Denel Rooivalk (“Red Kestrel”) is a twin-engine, tandem-seat attack helicopter manufactured by Denel Aviation of South Africa. Developed from the dynamic components of the Aérospatiale Super Puma/Atlas Oryx, it was designed for anti-armour, ground suppression, and anti-helicopter missions, tailored to operate effectively in the harsh African environment with minimal support.

Property Typical Value
역할 Attack Helicopter / Anti-Armour
제조업체 Denel Aviation (South Africa)
First Flight February 11, 1990
승무원 2 (Pilot and Weapon Systems Officer, in stepped tandem)
Main Rotor Diameter 15.58 m (51 ft 1 in)
Length (overall) 18.73 m (61 ft 5 in)
Max Takeoff Weight 8,750 kg (19,290 lb)

Design and Powerplant

  • Engines: Two Turbomeca Makila 1K2 turboshaft engines.
  • Power Output (each): Approximately 1,420 kW (1,904 shp).
  • Rotor System: Four-blade main rotor and a five-blade tail rotor.
  • Design Features: Features a crash-resistant structure, low radar, visual, infrared, and acoustic signatures, and fixed wheeled undercarriage.
  • Avionics: Equipped with an advanced navigation suite (Doppler Radar, GPS), an electronic countermeasures suite (chaff and flare dispensers), and a nose-mounted gyro-stabilized sensor turret (TDATS) for targeting and tracking.
  • Cockpit: Stepped tandem cockpits with armour protection and a Thales TopOwl Helmet-Mounted Sight and Display (HMSD) system.

Performance and Armament

  • Maximum Speed: Up to 309 km/h (193 mph, 167 knots).
  • Cruise Speed: 278 km/h (173 mph, 150 knots) at sea level.
  • Service Ceiling: 6,100 m (20,000 ft).
  • Combat Range: Approximately 740 km (380 nautical miles) with internal fuel.
  • Rate of Climb: Approximately 13.3 m/s (2,620 ft/min).
  • Fixed Armament: One F2 20 mm cannon mounted beneath the nose (700 rounds).
  • External Hardpoints: Six underwing hardpoints for a total external ordnance load.
  • Typical Armament Options:
    • Anti-Tank: 8 or 16 Mokopa ZT-6 long-range anti-tank guided missiles (ATGM) (or Hellfire/HOT 3 missiles).
    • Air-to-Air: MBDA Mistral or Denel V3C Darter air-to-air missiles.
    • Rockets: 38 or 76 70 mm folding fin aerial rockets (FFAR).

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