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Combat aircraftIn development
Air superiority fighter Technology demonstrator
Sukhoi Su-37 is a air superiority fighter Technology demonstrator originating in Russia.
RussiaTechnical data
True scale
Sourced dimensions beside a 1.75 m human reference.
Points represent sourced observations, including revisions. Revisions on the same effective date are not separate inventory events. Ranges appear in the table and are not plotted as exact points.
| Observation / report period | Value | Source | Claim state |
|---|---|---|---|
| 28 Sept 2026 | 21.935 m | Wikipedia contributors | superseded |
Air superiority fighter Technology demonstrator
Russia
Sukhoi Design Bureau
Komsomolsk-on-Amur Aircraft Production Association
Out of service and production, prototype, crashed in 2002
1
25 October 1997
2 April 1996 ( 1996-04-02 )
Sukhoi Su-30MKI (India) Sukhoi Su-30MKM (Malaysia) Sukhoi Su-30SM (Russia) Sukhoi Su-35 (Russia and China)
1
21.935 m (72 ft 0 in)
14.698 m (48 ft 3 in)
5.932 m (19 ft 6 in)
62 m 2 (670 sq ft)
18,500 kg (40,786 lb)
34,000 kg (74,957 lb)
2 × Saturn AL-37FU afterburning turbofan engines, 83 kN (19,000 lbf) thrust each with axisymmetrical thrust-vectoring nozzles dry, 142 kN (32,000 lbf) with afterburner
2,500 km/h (1,553 mph, 1,350 kn) at high altitude
3,300 km (2,100 mi, 1,800 nmi) at high altitude 1,390 km (860 mi; 750 nmi) at sea level
18,800 m (61,700 ft)
230 m/s (45,000 ft/min)
1× 30 mm GSh-30-1 internal cannon with 150 rounds
12 hardpoints, consisting of 2 wingtip rails, and 10 wing and fuselage stations with a capacity of 8,000 kg (17,630 lb) of ordnance .
+ 9
The sole example built was originally the eleventh Su-27M (T10M-11) built by the Komsomolsk-on-Amur Aircraft Production Association before having thrust-vectoring nozzles installed.
Reference text from Wikipedia contributors, used under CC BY-SA 4.0.
Sukhoi Su-37 equipment records. Variants, orders and quantities are shown as reported in each inventory source; coverage is incomplete.