Sukhoi Su-24MK

Explore the Sukhoi Su-24MK in side view and top view to compare its silhouette and proportions.

Sukhoi Su-24MK, side profile
Sukhoi Su-24MK, side profile
22.53 m
Sukhoi Su-24MK, top view, same scale
Sukhoi Su-24MK, top view
17.64 m

From Wikipedia

The Sukhoi Su-24 is a supersonic, all-weather tactical bomber developed in the Soviet Union. The aircraft has a variable-sweep wing, twin engines and a side-by-side seating arrangement for its crew of two. It was the first of the USSR's aircraft to carry an integrated digital navigation/attack system.

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Summary of “Sukhoi Su-24” 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-24MK by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/SU24/), CC BY 4.0

Specifications

Length
22.53 m
Wingspan
17.64 m
Max take-off weight
43.76 t
Max speed
1,654 km/h
Range
2,775 km
Ceiling
11,000 m
Engines
2 × Lyulka AL-21F-3A turbojet engines
Power
75 kN (17,000 lbf) thrust each dry, 109.8 kN (24,700 lbf) with afterburner
First flight
1967
In service
1974

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