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SU25

Su-25
by SUKHOI

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Performance

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Take-off

V2 (IAS) 130 kts

Distance 650 m

WTC M

RECAT-EU Lower Medium

MTOW 20500 kg

Initial climb (to 5000ft)

IAS 160 kts

ROC 1200 ft/min

Climb (to FL 150)

IAS 260 kts

ROC 6000 ft/min

Climb (to FL 240)

IAS 260 kts

ROC 500 ft/min

MACH climb

MACH 0.64

ROC 2000 ft/min

Cruise

TAS 350 kt

MACH 0.75

Ceiling FL 220

Range 800 NM

Initial Descent (to FL 240)

MACH no data

ROD 7000 ft/min

Descent (to FL 100)

IAS 300 kt

ROD 5000 ft/min

Approach

IAS 250 kt

ROD 1500 ft/min

MCS no data kt

Landing

Vat (IAS) 170 kt

Distance 750 m

APC E

Type of Aircraft

Type

L2J

APC

WTC

RECAT-EU

Lower Medium

Technical

Wing Span

14.5 m

Length

15.4 m

Height

5.2 m

Power plant

2 x 44,2 kN Soyuz Fumansky R-195 turbojets.

Performance Similarity

No data

Recognition

Wing position

High wing

Engine position

Both sides of fuselage

Tail configuration

Regular tail, mid set

Landing gear

Tricycle retractable

Recognition similarity

No data

Supplementary

IATA

no data

Accommodation

One pilot (two in tandem position in Su-25UB).

Notes

Close support and ground attack aircraft. In service since 1984. Designed specifically for close air support missions. From first flight in 1975 to first Su-25 unit were operational in 1984 a number of modifications were done. The Su-25 features titanium cockpit armouring and wingtip-pod airbakes. Built in many versions: Su-25K export version, Su-25UB and export Su-25UBK two seats version, Su-28 advanced trainer and Su-39 anti-tank version with new NAV system and laser range finger in the nose. Used by Russia and many East European Air Forces.

Alternative names

Su-28
Su-39
SUKHOI Su-25/28/39
Su-25/28/39
Frogfoot