Sukhoi Su-25/Su-25K (late production)

Explore the Sukhoi Su-25/Su-25K (late production) in side view and top view to compare its silhouette and proportions.

Sukhoi Su-25/Su-25K (late production), side profile
Sukhoi Su-25/Su-25K (late production), side profile
15.53 m
Sukhoi Su-25/Su-25K (late production), top view
Sukhoi Su-25/Su-25K (late production), top view
14.36 m

From Wikipedia

The Sukhoi Su-25 Grach is a subsonic, single-seat, twin-engine jet aircraft developed in the Soviet Union by Sukhoi. It was designed to provide close air support for Soviet Ground Forces. The first prototype made its maiden flight on 22 February 1975. After testing, the aircraft went into series production in 1978 in Tbilisi in the Georgian Soviet Socialist Republic.

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Summary of “Sukhoi Su-25” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.

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Drawing of the Sukhoi Su-25/Su-25K (late production) by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/SU25/), CC BY 4.0

Specifications

Length
15.53 m
Wingspan
14.36 m
Max take-off weight
19.3 t
Max speed
975 km/h
Range
1,000 km
Ceiling
7,000 m
Engines
2 × Soyuz/Tumansky R-195 turbojet engine
Power
44.18 kN (9,930 lbf) thrust each
First flight
1975
In service
1981

From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.