Su-25KM Scorpion [Georgia]

Crew	1 man
Length	15,53 m
Roll	14,36 m
Height	4,80 m
Net wing area	m2 30,10
Weight of an empty aircraft	kg 9100
Takeoff weight	Normal, kg 14520 - Maximum, kg 17500
Landing weight:	- Normal, kg 11000 - Maximum, kg 12100
Maximum military load	kg 4500
Supply of the fuel produced in internal tanks	3660 liters
Capacity of additional fuel tanks	???-800 (4 pcs.), l 820 each
Capacity of additional fuel tanks	???-1150 (2 pcs.), l 1160 each
Type and number of engines	2 ??? ?-195
Emergency traction force	, kg.force 2 ? 4500
Practical ceiling	m 7000
Maximum speed	- At the ground, km/h 950 - At height, km/h ?=0.82
Practical range ability	- At the ground, km/h 495 - At height, km/h 1000 - From 4????-800, km 1980
Takeoff roll	- With normal takeoff mass, m 500 - With maximum takeoff mass, m 1050
Landing roll	- With normal landing mass, m 550 - With maximum landing mass, m 750
Maximum working load +6,5/-2,0
Armament
Gun armament	Add-in (integrated) gun device ???-17?, double-tube with 30-mm gun ??-30, supply of 250 bullets Demountable gun device (4 pcs.) ????-22-01, double-tube with 30-mm gun ??-30, supply of 260 bullets each
Missiles armament	Air-to-air guided missiles ?-60 (?-60?), ?-73 Air-to-ground (air-to-surface) guided missiles ?-25??, ?-25?, ?-29? Unguided shells ?-5, ?-8, ?-13, ?-24, ?-25
Bomber armament	Aerial bombs 100, 250, 500 Incendiary tanks ??-500 Containers for small freights ????-2 Single-mission bomb cartridges ???-250, ???-500
Number of suspension centers	10

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