
Originally Posted by
Suhoij
Yes you right the km is a mod... of some Su which was made in Georgia maybe in 1991.
In the last years georgia didnt build only 1 of them.
Georiga built 4 SU-25s and upgraded them to SU-25KMs in 2007. Who told you that TAM cancelled production ? - Simply noone.
Fighter SU-25K
General
Developer: The P. Suhoi Design Bureau
SU-25K (commercial models (a) and (b)) has been produced by the Plant commercially since 1984. Over 210 aircrafts have been built up to present.
SU-25K (model a) was exported to the countries to Warsaw Agreement and Su-25K (model b) was exported to the developing countries. At present, it is included in the armaments of Czech Republic, Slovakia, Bulgaria, Hungary, Macedonia, North Korea, Angola, Iraq, Syria, Iran, Georgia, Congo, Azerbaijan, Ethiopia, Gambia and other countries.
Designation
Designation of the army fighter is to render direct support of infantry and to destroy small-size moving and immovable targets on the battlefield at night and by day, in terms of visual vision.
Typical enemies of the aircraft are as follows:
· Tactical missiles and artillery at firing positions, at marches and in the areas of concentration
· Tanks and motorized infantry in fighting or pre-fighting or marching state, at the points of support and in the areas of concentration
· Management elements of infantry, army tactical aviation
· Army aviation helicopters (airplanes) on squares and in the air
· Fire sections and anti-aircraft means.
Tactical-technical characteristics
Crew
1 man
Geometric characteristics
Aircraft dimensions:
- Length, m
15,53
- Roll, m
14,36
- Height, m
4,80
Net wing area, m2
30,10
Weight specifications
Weight of an empty aircraft, kg
9500
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, l
3660
Capacity of additional fuel tanks ПТБ-800 (4 pcs.), l
820 each
Capacity of additional fuel tanks ПТБ-1150 (2 pcs.), l
1160 each
Power plant
Type and number of engines
2 ТРДР-195 (for the first Р-95Ш)
Emergency traction force, kg.force
2 х 4500 (2 х 4100)
Flight-technical specifications
Practical roofing, m
7000
Maximum speed:
- At the ground, km/h
950
- At height, km/h
М=0.82
Practical range ability:
- At the ground, km/h
495
- At height, km/h
1000
- From 4хПТБ-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
ВПУ-17А, double-tube with 30-mm gun ГШ-30, supply of 250 bullets
- Demountable gun device (4 pcs.)
СППУ-22-01, double-tube with 30-mm gun ГШ-30, supply of 260 bullets each
Missiles armament:
- Air-to-air guided missiles
Р-60К (Р-60МК)
- Air-to-ground (air-to-surface) guided missiles
Х-25МЛ, С-25Л, Х-29Л
- Unguided shells
С-5, С-8, С-13, С-24, С-25
Bomber armament:
- Aerial bombs
100, 250, 500
- Incendiary tanks
ЗБ-500
- Containers for small freights
КМГУ-2
- Single-mission bomb cartridges
РБК-250, РБК-500
Number of suspension centers
10
Briefly about the aircraft
The aircraft is a subsonic monoplane with low height and for 1-person crew. Its active service has been increased and its maneuvering specifications are favorable at low speeds.
The aircraft may be exploited from concreted runaway and ground airfields, as well as from the airfields located in high mountains (at 3000 m above sea level).
The cockpit is armored and is equipped with conditioning and ventilation systems. The cockpit is equipped with an oxygen caddy for the pilot and an ejection seat.
The radio equipment of the aircraft provides a pilot’s communication to the overhead objects and aircrafts in every range of operational height and radius of the aircraft and transfer of the identification signals. The aircraft is equipped with short range and long range radio navigation systems allowing flying and landing at any time during the day and night, both in favorable and unfavorable meteorological conditions.
The sight system of the aircraft enables to destroy the target in terms of visual vision.
The weapon control system may be used to prepare and select the weapon and the mode of its application, as well as to control explosives and other elements of the aviation weapon in terms of different loads of the aircraft.
A filming equipment and photo-control device installed on the aircraft serve the purpose of controlling the results of gun firing and missile launch.
The aircraft safety system includes the apparatus identifying the functioning radar stations, automatic machine identifying passive infrared defects and dipole scatterers.
The most important peculiarities of the aircraft are:
· Higher life cycle than that of the aircrafts of front aviation at the expense of a complex of special means
· Powerful missile, bombing and artillery armament
· Little time necessary for preparation for a repeated flight, even in case the variant of armament is changed
· Relative simplicity of piloting techniques
· High exploitation produceability of the aircraft
· Capability of carrying out independent military actions even from the ill-equipped airfield
· High reliability of equipment, aggregates and systems
· Favorable vision from the pilot’s cockpit.
Fighter SU-25KM (Scorpion)

Developer: Elbit Systems Ltd. (Israel), TAM-TBILISI AIRCRAFT MANUFACTURING (Georgia)
SU-25KM (commercial model, modernized) has been produced by the Plant since 2001. The first aircraft took off on April 14, 2001. Total 6 aircrafts have been modernized.
SU-25KM is included in the military-air force armament of Georgia and Turkmenistan.
Modernization purposes
The modernization of SU-25KM aims at improving the military capabilities and widening the area of application of the aircraft, as well as reducing its performance expenses.
· Reaching conformity with NATO systems
· Reaching conformity with ICAO systems
· Exploitation of the aircraft at night and in unfavorable meteorological conditions
· Increasing the accuracy of application of the aviation annihilation systems (aerial bombs, unguided jet missiles) by approximately 2,5-3 times
· Boosting the efficiency of the aircraft application in air battles by approximately 2,5-3 times
· Improving flight safety at the expense of algorithms and verbal warnings
· Increasing the time of location above the target by 20% at the expense of the flight track optimization
· Ensuring training and education abilities by using Western concepts (using video records instead of photo an film-control apparatus)
· Ensuring the exploitation of a wider range of aviation facilities
· Increasing the reliability of the systems
· Reducing the load on the pilot by reducing the number of switches and instruments in the cockpit and by means of color displays and digital cards
· Reducing costs of performance by using Western technologies
· Reducing the time needed for preparation of the aircraft for flight.
Tactical-technical characteristics
Crew
1 man
Geometric characteristics
Aircraft dimensions:
- Length, m
15,53
- Roll, m
14,36
- Height, m
4,80
Net wing area, m2
30,10
Weight specifications
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, l
3660
Capacity of additional fuel tanks ПТБ-800 (4 pcs.), l
820 each
Capacity of additional fuel tanks ПТБ-1150 (2 pcs.), l
1160 each
Power plant
Type and number of engines
2 ТРДР-195
Emergency traction force, kg.force
2 х 4500
Flight-technical specifications
Practical roofing, m
7000
Maximum speed:
- At the ground, km/h
950
- At height, km/h
М=0.82
Practical range ability:
- At the ground, km/h
495
- At height, km/h
1000
- From 4хПТБ-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
ВПУ-17А, double-tube with 30-mm gun ГШ-30, supply of 250 bullets
- Demountable gun device (4 pcs.)
СППУ-22-01, double-tube with 30-mm gun ГШ-30, supply of 260 bullets each
Missiles armament:
- Air-to-air guided missiles
Р-60 (Р-60М), Р-73
- Air-to-ground (air-to-surface) guided missiles
Х-25МЛ, С-25Л, Х-29Л
- Unguided shells
С-5, С-8, С-13, С-24, С-25
Bomber armament:
- Aerial bombs
100, 250, 500
- Incendiary tanks
ЗБ-500
- Containers for small freights
КМГУ-2
- Single-mission bomb cartridges
РБК-250, РБК-500
Number of suspension centers
10
Briefly about avionics
Aircraft SU-25KM is equipped with modern aviation radioelectronics, with the technology “glass cockpit”, modernized navigation system and armament control system.
The complex of avionics fully operates on a modular multi-role computer MMRC (Modular Multi-Role Computer) produced by Elbit Systems Ltd., which is connected up with two bars of data exchange, type 1553B.
The cockpit has been thoroughly modernized. Most of analog devices have been replaced by two multifunctional 6' x 8'–size color displays MFCD (multifunction color displays). There has been a system HOTAS (Hands-On-Throttle-And-Stick) enabling a pilot to perform multiple operations without removing his hands off the control levers of the engines and aircraft installed. A display system on the windshield has been replaced by a new system with the control panel HUD (Head Up Display).
The complex includes a new navigation system, which works both in GPS and inertia modes. The radio equipment of the aircraft control also includes the landing system VOR/ILS. The navigation information is expressed on the color display as a moving map. There are two new frequencies – UHF and VHF installed providing the communication without any danger of unauthorized intervention.
The aircraft is also equipped with a state identification friend or foe (IFF) meeting the NATO standards.
Modernization of a fighter Su-25Km is carried out together with capital repairs resulting in the increased resource and life cycle of the aircraft.

Before modernization After modernization
Is there anything about cancelled productions ?