Sukhoi OKB - Russia / Soviet Union
Manufacturer(s)
Russia; Soviet Union
Operators
1997
Service Year
Russia
National Origin
Retired
Project Status
1
Crew
4
Units
X-PLANE
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
74.1 ft
(22.60 meters)
Length
49.7 ft
(15.16 meters)
Width/Span
20.7 ft
(6.30 meters)
Height
36,101 lb
(16,375 kilograms)
Empty Weight
77,162 lb
(35,000 kilograms)
Maximum Take-Off Weight
+41,061 lb
(+18,625 kg)
Weight Difference
2 x Aviadvigatel D-30F6 thrust-vectoring digitally-controlled afterburning turbojet engines developing 32,000 lb thrust each with afterburner.
Propulsion
1,684 mph
(2,710 kph | 1,463 knots)
Max Speed
59,055 ft
(18,000 m | 11 miles)
Ceiling
2,051 miles
(3,300 km | 1,782 nm)
Range
764 ft/min
(233 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
None. This was a technology demonstrator. Production-quality models may have featured an internal 30mm cannon and underwing/underfuselage hardpoints for munitions and fuel stores.