• First flight16 December 1994
  • Introduction1991–1996 2012–2015
  • StatusOperational
  • Number built2 prototypes

History

The Antonov An-70 (Ukrainian: Антонов Ан-70) is a four-engine medium-range transport aircraft, and the first aircraft to take flight powered only by propfan engines. It was developed in the late 1980s by the Antonov Design Bureau to replace the obsolete An-12 military transport aircraft. The maiden flight of the first prototype took place in December 1994 in Kyiv, now independent Ukraine. Within months the prototype had suffered a mid-air collision. A second airframe was produced to allow the flight-test programme to proceed. Both prototypes were produced by the Kyiv Aircraft Production Plant.

Following the dissolution of the Soviet Union in the early 1990s, the programme became a joint development between Russia and Ukraine. The former compounded the issue of a reduced market with its intermittent commitment to the project. Repeated attempts to start production have had limited success. Western European countries, including Germany, at one stage assessed the aircraft for procurement, but many later decided against it.

Development

Origins and early testing history

The origins of the An-70 can be traced back to the mid-1970s, when the Antonov Design Bureau began preliminary design work on a successor for the An-12 four-engine turboprop aircraft.[1] The Soviet Armed Forces, by the 1980s, were looking for a replacement for the An-12 and a complement to the Ilyushin Il-76 four-engine jet transporter; in 1987, the Ministry of Defence, with a new emphasis on air mobility, specified an aircraft with a quick loading time, the ability to operate from short unprepared airfields, could carry up to 300 troops, and have good operating economy.[2][3][4] The initial contract for work on the An-70 was concluded in May 1989;[5] Antonov began advanced design work on the new aircraft during the same year.[3] After the collapse of the Soviet Union, in June 1993, the Russian and Ukrainian governments agreed to jointly develop the An-70, with 80 percent of the funding expected to come from Russia.[6] The following year, twenty companies and organisations from the former Soviet Union agreed to jointly develop, market and support the aircraft.

Technical data

Specifications

01

Crew & dimensions

Crew
3–4 flight crew (two pilots and flight engineer (optional navigator)) + loadmasters and cargo attendants
Length
40.73 m (133 ft 8 in)
Wingspan
44.06 m (144 ft 7 in)
Height
16.38 m (53 ft 9 in)
02

Performance

Maximum speed
780 km/h (480 mph, 420 kn) Cruise speed: 750 km/h (470 mph, 400 kn) at 9,100–11,000 m (29,900–36,100 ft) 800 km/h (500 mph; 430 kn) max
Range
1,350 km (840 mi, 730 nmi) with 47,000 kg (103,617 lb) payload from 1,800 m (5,900 ft) runway 3,800 km (2,400 mi; 2,100 nmi) with 38,000 kg (83,776 lb) payload from 1,800 m (5,900 ft) runway 5,000 km (3,100 mi; 2,700 nmi) with 30,000 kg (66,139 lb) payload from 1,800 m (5,900 ft) runway 7,400 km (4,600 mi; 4,000 nmi) with 20,000 kg (44,092 lb) payload from 1,800 m (5,900 ft) runway 8,000 km (5,000 mi; 4,300 nmi) with maximum fuel from 1,800 m (5,906 ft) runway (STOL operations with reduced range)
Service ceiling
12,000 m (39,000 ft)
03

Powerplant

Powerplant
14-bladed Aerosyla Stupino SV-27, 4.5 m (14 ft 9 in) diameter contra-rotating propeller (8-bladed forward; 6-bladed rear)