
History:
The An-72 Coaler is designed as
a Short Take-Off and Landing (STOL) aircraft which can operate
from small unprepared airfields. The An-72 was first named as
An-32 and had propeller engines, but was later fitted with jet
engines. The first prototype flew end of 1977, and the aircraft
finally entered service in 1979.
The wings are high-mounted and back-tapered with blunt tips and
a negative slant. Two turbofan engines are mounted in long pods
on top of the wings, which makes this plane easily identifiable.
The engines are placed on the forward edge of the wings to increase
lift for STOL capability. To protect the wings, the jet exhausts
are blown over titanium panels on the upper surface. Such a position
of the engines also gives good protection against threats from
the ground. The fuselage is circular with a round, solid nose
and an upswept rear section. In the aft, there is a hinged loading
ramp from which up to 7.5 tons can be airdropped, and there are
folding side seats for 42 fully equipped paratroopers or 52 normal
passengers. The An-74 is based on the An-72, but has improved
avionics and radar together with an extended wingspan and an increased
range. It was especially designed to operate in the polar regions
where it can land on ice floes for resupply troops or rescue work.
Similar aircrafts are the C-160 Transall and the G.222.
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|
Function: |
Medium-transport with STOL
capability |
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Dimensions (wingspan/length/height): |
25.8 m / 26.6 m / 8.2 m |
|
Weight: |
26,500 kg takeoff weight (30,500
kg max.) |
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Engines: |
2 Lotarev D-36 with 62.8 kN
thrust each |
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Cruising speed: |
720 km/h |
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Landing speed: |
165 km/h |
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Airfield takeoff roll: |
400-450 m |
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Airfield landing roll: |
350-400 m |
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Range: |
3200 km max. (unloaded); 1200
km with max. payload |
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Ceiling: |
8000 m cruise (11000 m max.) |
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Armament: |
None |
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Crew: |
3 |
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Payload: |
32 passengers or 5000 kg of
cargo |
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Manufacturer: |
Antonov; Russia |