Sukhoi OKB - Soviet Union
Manufacturer(s)
Russia; Soviet Union
Operators
1984
Service Year
Soviet Union
National Origin
Active
Project Status
1
Crew
20
Units
22.3 ft
(6.80 meters)
Length
25.6 ft
(7.80 meters)
Width/Span
9.5 ft
(2.89 meters)
Height
1,543 lb
(700 kilograms)
Empty Weight
1,742 lb
(790 kilograms)
Maximum Take-Off Weight
+198 lb
(+90 kg)
Weight Difference
monoplane / low-mounted / straight, tapered
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Low-Mounted
Mainplanes are low-mounted along the sides of the fuselage.
Straight
The planform involves use of basic, straight mainplane members.
Straight, Tapered
The planform uses straight mainplane members which taper towards the wing tips.
1 x Vedeneyev M14P 9-cylinder air-cooled radial piston engine developing 360 horsepower and driving a three-bladed propeller unit at the nose.
Propulsion
280 mph
(450 kph | 243 knots)
Max Speed
13,123 ft
(4,000 m | 2 miles)
Ceiling
497 miles
(800 km | 432 nm)
Range
3,545 ft/min
(1,081 m/min)
Rate-of-Climb
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