Antonov - Soviet Union / Ukraine
Manufacturer(s)
Libya; Russia; Soviet Union; Ukraine; United Arab Emirates; United Kingdom
Operators
1986
Service Year
Soviet Union
National Origin
Active, Limited
Project Status
4
Crew
55
Units
TRANSPORT
General transport functionality to move supplies/cargo or personnel (including wounded and VIP) over range.
226.7 ft
(69.10 meters)
Length
240.5 ft
(73.30 meters)
Width/Span
68.2 ft
(20.78 meters)
Height
385,809 lb
(175,000 kilograms)
Empty Weight
892,872 lb
(405,000 kilograms)
Maximum Take-Off Weight
+507,063 lb
(+230,000 kg)
Weight Difference
monoplane / high-mounted / swept-back
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
High-Mounted
Mainplanes are mounted at the upper-most position allowable along the dorsal line of the fuselage.
Swept-Back
The planform features wing sweep back along the leading edges of the mainplane, promoting higher operating speeds.
4 x Ivchenko Progress D-18T turbofan engines developing 51,600 lb of thrust each.
Propulsion
537 mph
(865 kph | 467 knots)
Max Speed
39,370 ft
(12,000 m | 7 miles)
Ceiling
9,756 miles
(15,700 km | 8,477 nm)
Range
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030