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General information | |
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Type | Military transport aircraft |
National origin | Soviet UnionRussia / Ukraine |
Designer | Antonov Design Bureau |
Built by | Antonov Serial Production Plant Kazan Aircraft Production Association |
Status | Completed state tests, open for production |
Number built | 2 prototypes |
History | |
Manufactured | 1991–19962012–2015 |
First flight | 16 December 1994 |
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.
The An-70 is a monoplane with a high-mounted wing design that features four distinctive propfan engines. Designed by the Progress Design Bureau, each of the D-27 engines is rated at 13,800 shp (which can be uprated to 16,000 shp), which is used to drive the SV-27 contra-rotating scimitar propellers designed by Aerosila; eight on the front propeller and six on the aft propeller. The propfan engines deliver slipstream to the supercritical wings that feature double-slotted trailing edges to provide high lift coefficients at low speeds. The modernisation of the aircraft during 2010–12 saw upgrades to the engines, including the incorporation of FADEC, and the further separation of the two propellers: 16 The aircraft's cruise speed is 750 km/h (405 kt) at an operational altitude of 8,600 to 9,600 m (28,200 to 31,500 ft); Antonov claimed in 1997 that the aircraft had a design maximum speed of 850 km/h (460 kt, or Mach 0.8), which would have compared favourably with Mach 0.77 of the larger turbofan-powered C-17. According to DASA's evaluation, the propfan engines were 10 percent more efficient than conventional turboprops.
Ceiling
Combat RANGE
Aircraft Speed
Max Crew
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Similar to the An-124, the An-70 design makes extensive use of titanium and composites to keep weight to a minimum and increase damage resistance. Approximately 25 percent of the airframe is made of carbon-fibre composites, which are primarily used on control surfaces and the tail assembly, while aluminium and steel alloys are used for the rest of the structure.
The An-70 has a designed life of 45,000 hours over 15,000 flights.
The prototypes had a fly-by-wire flight-control system that comprised three digital channels and six analog channels.