SU-25

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.

Sukhoi

Type

Close air support

Role

Soviet Union / Russia

Country of Origin

1978–present

Introduction

Over 1,000

Note

The Su-25 has a conventional aerodynamic layout with a shoulder-mounted trapezoidal wing and a traditional tailplane and rudder. Several metals are used in the construction of the airframe: 60% aluminium, 19% steel, 13.5% titanium, 2% magnesium alloy, and 5.5% other materials.

Early variants included the Su-25UB two-seat trainer, the Su-25BM for target-towing, and the Su-25K for export customers. Some aircraft were being upgraded to the Su-25SM standard in 2012. The Su-25T and the Su-25TM (also known as the Su-39) were further developments, not produced in significant numbers. The Su-25, and the Su-34, were the only armored, fixed-wing aircraft in production in 2007. Su-25s are in service with Russia, other CIS members, and export customers.

The technical characteristics ​​may have minor differences according to the different manufacturers of the given product. The manufacturers reserve the right to make changes to the specified parameters.

Crew: 1

Length: 15.53 m (including nose probe)

Wingspan: 14.36 m

Height: 4.8 m

Wing area: 33.7 m2

Empty weight: 9,800 kg

Gross weight: 14,440 kg

Max takeoff weight: 19,300 kg

Maximum speed: 975 km/h

Range: 1,000 km

Combat range: 750 km

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Type of packaging

1

Quantity per pack

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Number in a wooden case

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Dimensions of a wooden case

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Weight of the package

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Weight of wooden case

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Weight

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Volume m3

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UN Number

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Hazard Class

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