Something like: What were the main differences of the planned combat roles of these a/c? The tactics, survivability and need of support in the battlefield (fighter cover or such)? The ability to operate in difficult conditions, from short runways, with minimum maintenance? And of course, the usual comparison of the weapon systems and the aircraft themselves and other interesting discussion.
Although I understand where this description came from (Su-25 and A-10 have similar missions etc.) the real counterpart of A-10 never made it. It was designed by Ilyshin and designated Il-102. Il-102 was based on earlier Il-40 ground attack jet. This beast had similar to A-10 dimensions and performance (as opposite to speedy Su-25). Someone in this group suggested that Su-25 is more of AlfaJet or attack version of BAe Hawk than A-10. In some respect it supported by the fact that few trainer versions of Su-25 popped out recently, including navalized version. One of them, Su-28, is a demilitarized Su-25UB. The aircraft outperforms L-39 and was used in aerobatics displays and competitions. Su-25 is amazing plane, its unprepared field performance is incredible and overall design simplifies logistics greatly:
The weapon systems were progressively upgraded and there is a development of Su-25 with radar pod (MAKS'95 photographed by Ken Duffey). Latest modification (Su-39) has greater range and much more capable than Su-25.
The Gratch (The Rook) emblem carried by several VVS Su-25s | In service with VVS Su-25 received a nickname "Gratch" (The Rook). This comes from the birds ability to get the food out of hard to reach spots, which is very similar to plane's ability to destroy the hardened targets in hard to reach locations in the mountains. The Afghanistani mujahideens called Su-25 "The German Product" because of their initial disbelieve that something that efficient can be designed by Soviets. It was the most feared and respected fixed wing aircraft. The Soviet infantry called Su-25 "Rascheska" (The Comb) because loaded Su-25 with its ten pylons occupied with the payload, resembled the comb if viewed from below. The VVS staff called Su-25 "Konyok-Gorbunok" which is a fictional animal from one of the fairtales by Bazhenov. This character is more like a pony or some sort of a miniature horse, which looks ugly and small, but can outperform the bigger (and faster) stablemates. Czechoslovak Su-25's were nicknamed "Steam Locomotives". |
Frogfoot was designed as a CAS machine and made it's combat debut in the early 1980's during the Soviet action in Afghanistan. In 1984, it achieved full operational status, and CIS production ended between 1991 and 92.
Su-25 (Frogfoot A)
All of the Su25 series (Frogfoots? Frogfeet?) feature a 24mm welded titanium cockpit armor tub, an air mixing duct system to cool engine exhaust, and other survivability features like foam-filled fuel tanks and pushrod-actuated control surfaces. In addition, 256 flares or chaff packets are carried near the rear of the aircraft in the tailcone and above the engine exhausts. The laser designator and target indicating electronics are carried in the extreme nose.
Alexei Gretchikhine:
Trainers and latest versions of Su-25 are build at Ulan-Ude plant (Siberia). Original Su-25 line in Tbilisi, Georgia ended up being abroad after disintegration of the Soviet Union. Every Frogfoot from Ulan-Ude carries a Bear emblem.
Urban Fredriksson adds:
Sukhoi's Su-25TM will be developed by 1997 and is now designated Su-39. The Su-39 will carry a Kopyo-25 multi mode radar in a pod under the fuselage and in addition to the Vikhr and other ground attack and anti-ship missiles will be capable of carrying AAMs like R-27, R-27ER, R-60, R-73 and R-77. The IR signature has been lowered by about four times by the adoption of cooling intakes on the upper surface of aircraft and a new center body which masks hot turbine blades.
>It has two turbojet engines -- 39.23 kN Tumanskiy/Soyuz R-95 in early >production aircraft, 44.13 kN Tumanskiy/Soyuz R-195 engines in later >aircraft. Armament is a twin-barrel 30mm cannon with 250 rounds, and >up to 4400 kg (R-95 engines) or 6400 kg (R-195) payload on 10 underwing >hardpoints.Just a couple of comments. The Su-25T/TK version was originally supposed to go into service as the Su-34, but that was eventually given to the Su-27IB "Flanker" bomber variant, and the Su-25T's production designation is Su-39.>Dimensions: Length 15.53 m, wingspan 14.36 m >Weights: Empty 9500 kg, max t/o 17600 kg (R-95) or 19200 kg (R-195)
>Known variants: > (R-95 engines) > Su-25 -- Original production ground attack aircraft > Su-25K -- Export version of Su-25 > Su-25UB -- Two-seat combat trainer > Su-25UBK -- Export version of Su-25UB > Su-25UBP -- Naval trainer based on Su-25UB > Su-25UT -- Unarmed primary trainer (sometimes referred to as Su-28) > Su-25UTG -- Naval trainer based on Su-25UT > (R-195 engines) > Su-25BM -- Enhanced ground attack aircraft (this is the current > production version, and the most numerous in Russian > service) > Su-25T -- Proposed enhanced version with more armour, improved > sensors, and possibly a new gun and engines > Su-25TK -- Proposed export version of Su-25T
Despite an early report that the program had been canceled, the 1994-5 Jane's reported that about 20 are in service with the Russian VVS, and deliveries are continuing.
Second, the Su-25BM was only used as a weapons trainer and target tug, and is not a very numerous variant. The most numerous in-service variant is the original Su-25, with about 450 in VVS service and another 100-200 having been exported.
Finally, the original pre-production machines which were deployed to Afghanistan for operational trials in the early 1980s were designed T-8, the Sukhoi OKB designation. The Su-39 pre-production aircraft were called T-8M.
barbiero@nis.net (Andreas Barbiero) wrote:
Normal payload is close to 3100 lb (1400kg) and maximum load is 9700 lb (4400kg). Look up A-10 numbers and keep in mind that Su-25 is much smaller aircraft.
The protective measures of Su-25 represent 7.5% of normal take off weight (some 2415 lb (1095 kg)) which is comparable with A-10's 2887 lb (1310kg).
All vital controls are protected by armor. Flying controls are actuated via 40 mm diameter titanium rods that are proof against 12.7 mm strikes, and the pitch control rods are duplicated.
Here are few more stories highlighting Su-25 roughness:
-Major Rubalov's Su-25 was hit in the engine which surged and flooded an engine bay with fuel, the cockpit was shattered, buster controls are gone and major's face covered with blood. None of the dials in the cockpit worked and his wingman guided him to the final approach. After belly landing, major rushed away from the Su-25 fearing that plane going to explode. After figuring that this is not going to happen, he got back to the aircraft and cut the engine.
-Another Su-25 was on fire which burned out most of the wiring and 95% of horizontal tail controls. In few moments before the landing, fire short cut the gear release wires and Su-25 made "conventional" landing.
-Lieutenant Golubtsov's Su-25 lost half of its rudder along with breaks. After landing his a/c ended up off runaway and rolled into adjacent mine field. He was forced to wait in the cockpit till mine squad cleared his way out.
-One Su-25 brought a missile in the engine which failed to detonate. (SAM?)
-Rutskoi's Su-25 was hit by AAA (ZGU) when a missile (Blowpipe) hit right engine (head on - it "turned off" the engine though the intake). Second AAA finally managed to shot it down. This is a second Frogfoot he flew (not the preproduction T-8-15 Blue 15 which was damaged twice). Rutskoi spent some time as Pakistani POW and was shortly exchanged.