Antonov An-70

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Image:Antonow An 70 rvb jno MACS 2001 0037.03.jpg The Antonov An-70 is a next-generation four-engine medium-distance transport aircraft, and the first large aircraft to be powered by propfan engines. Developed by the Antonov design bureau to replace the obsolete An-12 military transport, work on the An-70 began in the early 1990s.

Maiden flight of the first prototype took place on December 16, 1994 in Kiev, Ukraine.

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History of production and marketing

Russia and Ukraine have (as of 2002) agreed on a 50-50 risk-sharing deal on production. Particularly, there were plans to establish serial production of the model in both Kiev and Samara, Russia, guaranteeing employment of about 80,000 people in two countries. The Russian government has shown interest in purchasing 160 planes for its military.

The first prototype was lost in 1995 during test flight. The second prototype suffered damage in a 2001 emergency landing during cold weather testing in Russia, but was repaired. Soon after the first crash, Russian authorities started to question the An-70's abilities and demanded further development.

In May 2005, senior officials of Russian Air Force claimed that bilateral development and further testing of the plane continue, though inside sources (Piort Butowski) report that the An-70 is rapidly losing ground to the upgraded IL-76MF, with the Tu-330 and IL-214 coming up strongly on the outside. In November 2005, Ukraine's Defence Ministry announced plans to buy five AN-70s for the Ukrainian Air Force. In December 2005, Antonov maintained that production of the aircraft remains a priority.

As of 2006, the plane was fully tested and internationally certified, though Russian and any potential Western customers have yet to purchase or invest in the serial production of the An-70.

Technology

Fully fly-by-wire, the An-70 features a glass cockpit and uses composite materials throughout. It is powered by four Progress D-27 turboprop engines, each turning a pair of contra-rotating propfans, and reaches 90% efficiency (claimed) in cruise at jet speeds.

Specifications (An-70)

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General characteristics

  • Crew: 3-5
  • Capacity: 300 troops, 206 wounded, or up to 47t cargo
  • Length: 40.7 m (133 ft 6 in)
  • Wingspan: 44.06 m (144 ft 7 in)
  • Height: 16.38 m (53 ft 9 in)
  • Wing area: m² ( ft²)
  • Empty: 66,230 kg (146,000 lb)
  • Loaded: 108,860 kg (240,000 lb)
  • Maximum takeoff: 130,000 kg ( lb)
  • Powerplant: 4x Progress D-27 propfans, 10,350 kW (13,880 hp)

Performance

  • Maximum speed: 780 km/h (420 knots)
  • Range: 8,000 km (4,320 nm) ferry flight, 6,600 km (3,600 nm) with 20t cargo
  • Service ceiling: 12,000 m (40,000 ft)
  • Rate of climb: m/min ( ft/min)
  • Wing loading: kg/m² ( lb/ft²)
  • Power/mass:

References

External links

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