- 1 -
Prototype of the Su-7.
- 2 -
Prototype of the Su-7. The S-2 was a little more refined than the S-1.
- S-21 S/21/S-21.jpg -
buisness class supersonic a/c.
VK-21 engines.
range 7400km.
speed 2M.
take-off mass 51,800kg.
Initially developed in alliance with Golfstream Aerospace.
Now talks in progress with Dassault Aviation.
Estimated price not more that USD50M per unit and USD1G for 2..5 years.
See also: http://www.avias.com/aviation/v466.html.
- S-22 -
see Su-7.
- S-22I -
Development of S-22 introducing variable (Izmenjaemaja) geometry.
Impact of this modification was great: with 50% more payload takeoff run
became twice as short and range twice as large. It was the prototype for the
Su-17.
- S-23 -
See Su-17.
- S-32 - First two (S-32-1 and S-32-2)
serial Su-17.
- S-37 Berkut 10.0K -
Length 22.6m.
X-wings. Wing span 16.7m.
Take-off weight 24t.
Max speed above 2200km/h.
Two engines of total thrust of 25t.
The a/c claimed to be a "stealth".
Designed to be a shipborn naval a/c (???).
The a/c expected to have no production due to political shit.
More: pic.1 8.5K, pic.2 33.7K, pic.3 10.0K, pic.4 52.1K,
Contributed.
Demo flight: pic.1 27.0K, pic.2 23.0K, pic.3 37.6K, pic.4 56.5K, pic.5 56.1K.
MACS'2001
Cyrillic text follows!
If you cannot read it click <HERE>
|
©«Коммерсантъ-Daily» No183, 24-Oct-1997
США и Россия борются за пальму первенства в разработке истребителя XXI
века, сочетающего качества сверхманевренной сверхзвуковой боевой
машины и самолета-невидимки, который не засекают радары и средства
инфракрасного наблюдения.Создание такого истребителя не только резко
утеличивает эффективность ВВС, но идает возможность получить важный
козырь в борьбе за мировой рынок вооружений. Как стало известно
корреспонденту "Коммерсанта-Daily" ЛЕОНИДУ ЗАВАРСКОМУ, ОКБ им. Су хого
проводит испытания такого истребителя, получившего название С-37
"Беркут".
До сих пор ведущие производители самолетов не могли соединить в одной
машине столь противоречивые с технологической точки зрения
характеристики. Причем Россия в большинстве случаев выступала в роли
догоняющего. Так, МиГ-29 создавался как ответ американскому
истребителю F-18, а Су-27 был противовесом американскому же F-15 .
Хотя эти самолеты и были большим достижением авиастроения, новые
военные доктрины требуют создания самолета, сочетающего в себе многие
качества "самолета-невидимки" (так называемая технология stealth,
недоступного радарам и приборам инфракрасного наблюдения и
многоцелевого сверхзвукового сверхманевренного истребителя.
Американский дозвуковой самолет-невидимка F-117 имеет очень скромные
летные данные и не может участвовать в воздушнык боях. ВВС США
затратили огромные средства на создание действительно боевого самолета
stealth (например, неудачный проект grumman Х-29), однако
приблизились к реализации этой цели только в сентябре 1997 года с
началом испытаний истребителя Lockheed-Martin F-22.
На этот раз американцы не могут рассчитывать на безусловное
первенство - ОКБ Сухого приступило к летным испытаниям С-37 "Беркут"
лишь на две недели позже американского конкурента. По оценкам
экспертов, "Беркут" превосходит F-22 в первую очередь за счет
уникального крыла обратной стреловидности. "Коммерсанту-Daily" стали
известны основные характеристики "Беркута". Длина 22,6 м, размах
крыла 16,7 м, взлетный вес 24 т, максимальная скорость свыше 2200
км/час. На самолете установлены два двигателя общей тягой 26 т, что
обеспечивает очень высокую энерговооруженность.
В США программа F-22 объявлена приоритетной. В России же в очередной
раз проявляется национальная специфика. С-37 "Беркут" создавался по
заказу Минобороны для ВВС. Однако, по имеющейся информации, на показе
самолета военным представители ВВС не присутствовали. Источники в
Минобороны утверждают, что дело в "сложном отношении" главкома ВВС к
генеральному конструктору ОКБ им.Сухого Михаилу Симонову.Но, по всей
видимости, есть и другие причины. "Коммерсанть-Daily" уже не раз
рассказывал о конфликтах вокруг ОКБ и попытках снять Симонова, Все это
- результат борьбы финансовых группировок (ОНЭКСИМбанка и Инкомбанка)
за контроль над финансовыми потоками как самого ОКБ, так и
создаваемого унитарного предприятия АВПК "Сухой", объединяющего
серийные авиазаводы и разработчиков самолетов Су. Так как влияние
финансовых группировок, имеющих виды на АВПК, велико, некоторые
военные по меньшей мере стараются быть крайне осторожными. На показ
прибыли только представители ПВО и авиации ВМФ.
Пока всемерную поддержку С-37 оказывают советник Бориса Ельцина по
авиации и космосу Евгений Шапошников. Проблемы военной авиации опять
не могут решиться в рамках соответствующихведомств, а за поддержку
президента опять ведется закулисная борьба.
Как бы то ни было, создание "Беркута" имеет огромное технологическое,
военное и политическое значение, и, главное, позволяет получить
хороший козырь в борьбе за мировой рынок вооружений XXI века.
Now it is renamed to Su-47.
- S-38 - agricultural project.
early name of Su-38.
Modifications:
- S-38L - agricultural.
One M337AK.1 engine of 210hp.
Normal takeoff mass 1200kg.
Up 400l of chemical agent.
Application speed 180..200km/h at 1..15m of altitude.
Assigned lifetime 3000 hours.
Estimated yearly flight 300 hours.
(From a Su's adv poster)
Sertification expected before year 2002.
Estimated price USD130K.
Estimated market 800..900 aircraft.
- S-52 - fifth generation fighter.
X-wing, foreplanes, thrust vectoring.
©«Indepedent Military Review» No28, 1997, p.3
Pre-flight test of the new top-secret fifth-generation fighter S-52
are conducted at Gromov LII in Zhukovski.
S-52 development was started at Sukhoy OKB in 1987.
Reverse arrow wing, two thrust-vectored engines, 17m wing span.
First flight planned for September 1997.
hm-hm..
S-37 has been flown in Zhukovski.
Probably, it is the "S-52".
-jno
- S-54 -
lightweight, single-engined trainer with Su-27 derived aerodynamics.
one R-195FS or RD-33 engine.
- S-55 -
refined version of S-54. competitor to MiG's "LFI"???
- S-56 8.3K -
development of S-55?
"MiG-21 for XXI century".
Looks like downsized Su-33 (twice less mass).
EDS about 0.2 to 0.5 sq.meters.
One AL-31F or AL-41F enfine.
"Sokol" (falcon) radar (diameter 980mm, active phased array, 30 targets tracked
at a time, fire against 6 targets at a time including hoovering helos,
resolution 3 meters at 25km). Maneurable overload 10..12.
9 points of undercarriage.
Missiles: RVV-AE, R-73, etc.
Wing span 11.23m. Length 15.3m. Take off mass 12t. Empty 7t. Fuel 4.5t. M=2.0.
Range without extra tanks 4000km. Ceiling 18km.
- S-62 - unmanned civil aviation vehicle for BAK-62 complex.
Development initiated in November 2002.
- S-80 32.4K - transport a/c.
Two engines from General Electric, 1,500hp each.
Produced by Kmsomolsk-na-Amure Aviation Amalgamation named after Y.Gagarin.
Estimated series: up to 150 aircraft for Russia plus up to 190 units for
export.
First one was delivered to Moscow in Jan'2000.
Practical range 1200km at 520km/h.
25 passengers (there are plans for 32-seat version).
Planned as a replacement for An-24, An-26, and An-28.
First S-80GP has been built in Komsomolsk-Na-Amure.
Certification expected by 2003.
More: pic.1 20.2K.
| C-80 Многоцелевой самолет | -
| S-80 Multirole aircraft
|
| Размеры:
| -
| Size:
|
| размах крыла, м
| 23,16
| wing span, m
|
| длина самолета, м
| 16,68
| Length
|
| высота, м
| 5,58
| height, m
|
| площадь крыла, м²
| 44
| wing area, m²
|
| Число мест:
| -
| Seats:
|
| экипажа
| 2
| pilots
|
| пассажиров
| 19-24
| passengers
|
| Размеры пассажирской кабины:
| -
| Passenger salon size:
|
| длина, м
| 6,3
| length, m
|
| максимальная ширина, м
| 2,15
| max width, m
|
| максимальная высота
| 1,9
| max height, m
|
Двигатели:
ТВД Дженерал Электрик СТ7-9 (2х1750л.с.)
или ТВД-1500 (2х1500 л.с.).
| -
| Engines:
General Electric CT7-9 (2x1750hp)
or TVD-1500 (2x1500hp).
|
| Диаметр шестилопастных воздушных винтов АВ-36, м
| 2,65
| Diameter of 6-blade propellers AV-36, m
|
| Массы и нагрузки (максимальные), т:
| -
| Masses and loads (max), t:
|
| взлетная
| 11
| take-off
|
| пустого снаряженного
| 6,5
| empty, refuelled
|
| платная нагрузка
| 3,1
| payload
|
| посадочная
| 10,4
| landing
|
| запас топлива, л
| 2500
| fuel, l
|
| Летные данные:
| -
| Flight data:
|
| крейсерская скорость, км/ч
| 480
| cruise speed, km/h
|
| дальность полета с максимальной платной нагрузкой (с резервами топлива), км
| 1250
| range with max payload and fuel reserve, km
|
| с максимальным запасом топлива, км
| 4500
| with max fuel load, km
|
| эксплуатационный потолок, м
| 8000
| practical ceiling, m
|
| потребная длина ВПП (условия МСА, на уровне моря), м
| 360
| required length of the runway (MCA conditions, at sea level), m
|
| Электронное оборудование:
| -
| Avionics:
|
|
На самолете используется цифровой комплекс авионики "Про Лайн" 2 (EFIS) фирмы
"Року-элл-Коллинз".
| -
| Digital system "Pro Line 2" (EFIS) from Rockwell-Collins.
|
| Уровень шума соответствует нормам ИКАО
| -
| Noise elevel conforms to IKAO regulations.
|
| Дополнительные сведения:
| -
| Extra data:
|
|
Разработка многоцелевого самолета С-80 началась в 1989 г. в ОКБ П. О. Сухого в
рамках конверсионной программы. Самолет предназначается для автономной
эксплуатации на неподготовленных аэродромах с ВПП длиной не более 400 м.
В середине 1996 г. между АО "Рыбинские моторы" и фирмой "Дженерал Электрик" было
подписано соглашение о выпуске в России двигателей СТ7-9 по лицензии и
использовании их на самолетах С-80.
Самолет С-80 имеет высокую скорость полета, может использоваться с коротких ВПП и
обладает высокой конкурентоспособностью на мировом рынке. Самолет обладает
автономностью эксплуатации за счет наличия ВСУ и имеет потенциальные возможности
дальнейшего совершенствования.
Кроме пассажирского варианта в "ОКБ П.О.Сухого" созданы:
- грузопассажирский вариант С-80ПГ,
- десантно-транспортный самолет С-80ТД,
- патрульно-транспортный самолет С-80ПТ,
- санитарный вариант С-80М,
- рыбопоисковый вариант С-80Р,
- самолет-носитель геологоразведочной аппаратуры С-80ГР.
|
|
The development of multirole aircraft S-80 has began in 1989 in Sukhoy OKB
as a conversion program. The a/c intended for autonomous exploitation from
unprepared runways not longer than 400 m.
AO "Rybinsk Motors" and "General Electric" has signed up an agreement to
start production of CT7-9 engines in Russia in 1996.
The S-80 a/c has high flight speed, can be used on short runways and has
high ability in competition on the world market. The a/c has the ability of
autonomous basing for being equipped with extra engine system and can be
enhanced as needed.
Besides the passenger version:
- S-80PG (or "GP") - cargo-passenger version
30 passengers or 3500kg payload.
max range 2890km.
cruise speed 535km/h.
ceiling 9000m
two ST7-9V engines by General Electric.
- S-80TD - transport/landing version
- S-80PT - patrol transport
- S-80M - medical version
- S-80R - fish detecting version
- S-80GR - geological recogissance version
|
- S-90 - passenger and cargo polymorphal aircraft.
Should be displayed at Gelendzhik-2000 expo (06..10-Sep-2000).
altitude 0.5 to 4000m.
range 3000km+.
Morphems:
- conventional aircraft - max weight 7900kg. payload 2500.
- WIG - max weight 9500kg. payload 3100.
- hydrofoil ship - max weight 10500kg. payload 4500.
- Su-7 32.8K Fitter [Designation reused!] -
The Su-7B 42.2K (bureau designation S-22) was a simple
ground attack aircraft, similar to a Su-9 with a swept wing replacing the delta
wing. Weapons load and range were limited, and the Su-7B wasn't that useful.
Iraq, Algeria and North Korea still operate few dosens of Su-7B's. One 10000kg
Lyulka AL-7F. 1956.
More: pic.1 40.5K, txt.2 [1.6K], pic.3 32.8K.
See also: Su-7 @ Wings of Motherland
The Su-7 in Indian AF Service. - Su-9/T-43 43.6K Fishpot [Designation reused!] -
Single-engine all-weather fighter. Su-9 has one 19,840 lb st (with AB)
Lyulka AL-7 turbojet. No cannon armament. Su-9 was similar to Su-7
fighter-bomber, but with a delta wing rather than the original swept wing.
The Su-9 (Design Bureau designation T-43) had the same configuration as the
MiG-21, a tailed delta, but was larger and heavier. It was a specialized
all-weather interceptor for the PVOS. Built in large numbers. 1959.
More: pic.1 39.7K.
Prototypes:
- ? Product-K [Type-8] -
early Me 262 copy; first seen 08/03/1947 Soviet Aviation Day, Tushino.
- T-1 - the first prototype
- T-3 - development of T-1, new inlet shape and housing of radars
- PT-7/T-7 - with variable geometry inlet
Modifications:
- Su-9B 12.5K -
- Su-9U Maiden -
Tandem, two-seat conversion trainer variant of Su-9 interceptor.
Developments:
- PT-8 -
- Su-11 -
new engine, radar, armament
- T-5 -
odd looking experimental version with two engines in flared out afterbody
fuselage
- T-37 - experimental aircraft
- T-49 - splitted intake to accomodate larger radar. Experimental
- T-431 - record setting version (??)
- Su-10 -
Four-engined jet bomber.
- Su-11/T-47 47.3K Fishpot [Designation reused!] -
Single-engine all-weather fighter, has one 22,050 lb st (with AB) Lyulka
AL-7F-1 turbojet. No cannon armament. Su-11 is uprated version of Su-9 with
more powerful engine, more advanced electronics and armament.
One 10000kg Lyulka Al-7F-1. 1967.
Prototypes:
- PT-8 -
- Product-LK [Type-17] -
modified Su-9; first seen 1949 Soviet Aviation Day, Tushino.
Modifications:
- Su-11U Maiden -
Tandem, two-seat conversion trainer variant of Su-9 interceptor.
Developments:
- T-37 - experimental aircraft
- Su-15/T-58 23.4K Flagon [Designation reused!] -
Single-seat all-weather interceptor Two 15,000 lb. st. (with AB) Tumanksy
R-13F-200 turbojets (Flagon E and F). No cannon armament. Four air to air
missiles under the wings.
The Flagon combined the tailed delta configuration of the Su-9 with twin engines,
side intakes and large radar nose. It was the first really capable all-wheater
interceptor of the PVO. The Su-15 became infamous when one shot down a Korean
Air Lines 747. Such incident was only a matter of time with the often rather
trigger-happy PVO... About trigger-happy guys see article at
Fair concerning USA and USSR
practice of shooting down civil planes.
Two 70.6kN Tumansky R-13F2-300. Retired in 1992. 1967.
IFF system SRZO-2M, SOD-57. By Off-Topic.
Modifications:
- Su-15 prototype Product-P [Type-18] -
first seen 1949 Soviet Aviation Day, Tushino
- Su-15 - "base"
- Su-15T - new nose gear weel (doubled)
- Su-15UT - Su-15T based 2-seats trainer, a bit longer
- Su-15TM - new ogival nose fin
- Su-15UM - Su-15TM based 2-seats trainer
- T-58L - with sky gear
- T-58VD - with extra take-off engines
More: pic.1 23.4K, pic.2 47.6K, pic.3 34.3K, pic.4 66.1K, pic.5 22.0K, pic.6 18.1K.
Wrong designation - Su-21.
- Su-17/S-23 40.3K Fitter [Designation reused!] -
The Su-17 (bureau designation S-23) was a large step in the development of the
Su-7B to a more useful attack aircraft. The most important change was the
introduction of swivelling outer wing panels, improving take-off and landing
performance, and thus allowing a larger weapons load.
Impact of this modification was great: with 50% more payload takeoff run
became twice as short and range twice as large.
IFF system SRO-2M, SOD-57. By Off-Topic.
One 11340kg Lyulka AL-21F-3. 1971.
©«Indepedent Military Review» No21, 1997, p.6
Aircraft: Su-17M4.
Take-off mass 16,400kg (max 19,500kg).
Combat load mass 4,250kg.
Fuel 4,000kg (with extra tanks 7,200kg).
Max speed at 11km 1,900km/h (at ground 1,350km/h).
Practical ceiling 15,200m.
Max overload 7.0.
Low altitude range 330km (with extra fuel tanks 650km).
Max distance 2,750km.
Length 19.02m.
Wing span 10.04/13.7m.
Wing area 34.5/38.49m².
Heigth 5.19m.
More: pic.1 54.5K, pic.2 40.3K.
Combat activity
- 2 (Su-17/Su-22) were lost in Afganistan in 1979..1988.
- Su-19 -
Designation used, in error, in old sources to refer to the Su-24.
- Su-20 Fitter -
Export version of the Su-17.
- Su-21 -
Su-27-derived supersonic bizjet project, now abandoned.
Designation reported for late model Su-15's. Seems to be incorrect.
- Su-22 30.9K Fitter -
Su-17, reengined with the Tumansky R-29B-S-300 turbojet. France and Russia
planned to display (did ?) an interesting upgrade proposal at the Paris airshow
at Le Bourget in June 1995 for this ageing plane.
More: pic.1 26.4K, pic.2 59.5K, pic.3 46.1K.
Combat activity
- 2 (Su-17/Su-22) were lost in Afganistan in 1979..1988.
- Su-24 28.4K Fencer -
Two-seat deep penetration interdictor and strike, reconnaissance and
electronic warfare aircraft. Two 25,350 lb. st.(with AB) Tumansky R-29B
turbojets. (Or two Saturn AL-21F-3A 76kN dry and 110kN on AB?)
One 30 mm cannon plus up to 13,000 lbs of external ordinance.
Design 1964. First flown in 1967. Entered service in 1974.
A variable geometry strike/attack aircraft, similar in its concept to the U.S.
F-111, but more optimized for the low-level tactical strike role. There also
are reconaissance versions. Two 110kN Lyulka AL-21F-3A. 1974.
570 in VVS (incl. 90 recce), 127 in VMF (incl. 20 recce).
24 sold to Iraq (now in Iran), 15 in Lybia, 20 in Syria.
Wrong, but wide spread designation: Su-19.
©«Indepedent Military Review» No21, 1997, p.6
Aircraft: Su-24M.
Take-off mass 35,910kg (max 39,700kg).
Combat load mass 8,000kg.
Fuel 9,800kg (with extra tanks 16,460kg).
Max speed at 11km 1,700km/h (at ground 1,400km/h).
Practical ceiling 11,000m.
Max overload 6.5.
Low altitude range 390km (with extra fuel tanks 570km).
Max distance 2,850km.
Length 24.594m.
Wing span 10.366/17.638m.
Wing area 51.0/55.16m².
Heigth 6.193m.
Dedicated page [3.6K].
Prototype: T-6 17.0K - fixed wing prototype;
note the down-turned wingtips.
Compare to TSR.2 75.4K ;-).
More: pic.1 79.6K, pic.2 69.1K, pic.3 23.0K.
Sold to: Iraq, ...
Combat activity
- Afganistan in 1979..1988. None were lost.
- Iraq. There were 30 Su-24 in 1998.
Modifications:
- Su-24 - frontline bomber. 1974.
- Su-24M - modernized Su-24. 1980.
- Su-24MR - tactical recce. 1984.
- Su-24MK - modernized export version of Su-24M. 1985.
- Su-24MP - AEW. 1986.
- Su-24MT - tanker. 1986.
- Su-24T - tanker. 1989?
- Su-24MM - more modernized (AL-31F engines). cancelled. 1985..1986.
- Su-25 16.1K Frogfoot -
Single-seat attack and close air support aircraft. Two 9340 lb. st. Tumansky
R-13-300 turbojets. One 30 mm cannon, plus up to 8820 lbs. of external
ordinance. Entered service in 1981-2.
Comparision [1.6K]
Heavily armoured attack and anti-tank aircraft. The Su-25 is a well-armoured
aircraft, capable of carrying a large load under its shoulder-placed wing. It
was extensively used in Afghanistan, and experience there led to major
improvements like titanium plate between engines. A navalized version was built
for the large carriers. Unarmored and unarmed version is an aerobatic jet Su-??.
Two 4000 kg Tumansky R-95 (R-195?). 1978.
More: pic.1 12.9K, pic.2 17.6K, pic.3 20.9K, pic.4 15.4K, pic.5 26.7K, txt.6 [16.1K], pic.7 29.6K, pic.8 38.0K, pic.9 148.7K, pic.10 64.7K, txt.11 [1.6K].
Modifications:
- Su-25T - I-251 automated seeker. First flown in August, 1984.
- Su-25TM 17.5K - with radar pod
- Su-25UB - trainer
- Su-25UBK - export trainer (Bulgary, Chechoslovakia, Hungary, Siria, Iraq, North Korea)
- Su-25UBP - trainer. replacement for Su-25UB.
- Su-25UTG 68.0K Frogfoot-B - Navy trainer (AKA Su-25K ?)
GSh-30-2 gun in turnable turret.
10 undercarriage points for 4360kg of load.
- Su-25K 15.9K - Navy trainer
- Su-25K 36.9K -
More: pic.1 93.4K, pic.2 29.2K.
- Su-25MC - modernized Su-25K.
Sometimes referred as Su-34 (designation reused!), another designation is Su-39.
Program discontinued. The screen on the upper right is the 360 degree Shkval laser
targeting system.
- Su-28 - trainer/aerobatic/export version
- Su-25TK 18.0K (September 18, 1996) -
Chechnia points to several long-term deficiencies in the VVS (Russian
Air Force) that must be addressed for it to remain a capable and effective
force. The conflict pointed to the age and ineffectiveness of much of its
older airframes like the Mi-24 and Su-25. The advanced targeting capabilities
of aircraft like the improved Su-25TK (shown here) have been sorely missed
in Chechnia; the older Su-25 `Frogfoots' proved unable to cope with bad
weather. If it were not for the Su-24, the VVS would have been unable to
conduct air operations for two months. See 'The Chechen Conflict' in Special
Report No 11. Special Reports are part of the Jane's Intelligence Review
subscription package. 1996.
Su-25TK is capable to utilize X-58 and X-31P anti-radar missiles,
X-25ML and S-25L laser guided missiles,
anti-tank missile system "Vikhr" ("Vortex"),
air-to-ground 80..370mm rockets,
free-fall and guided bombs,
heat-seeking air-to-air missiles,
new 30mm cannon.
- Su-25UB 15.4K/Su-25UTG - naval?
- Su-25? - w/40mm cannon. experimental.
Combat activity
- 23 were lost in Afganistan in 1979..1988.
- Su-26 77.4K -
aerobatic.
This airplane, a Sukhoi Su 26, is another participant to the 1995 Breitling
World Cup of Aerobatics. It was flown by Nikolay Timofeev.
Modifications:
- Su-32 - trainer [Designation reused!]
More: pic.1 63.0K.
- Su-27 72.4K Flanker -
single-seat air superiority fighter. Two 30,000 lb. st. (with AB) Lyulka RD-32
turbofans. One 30 mm cannon plus up to 10 air-to-air missiles. Landing speed 220km/h.
Entered service in 1986.
Minimal flying speed: 190-200km/h (shown by a service pilot), 170km/h (at 26 deg, shown by a test pilot).
Minimal take-off run: 400m. (As reported by a pilot.)
The Su-27 is a big long-range air superiority fighter, comparable to the U.S.
F-15 but superior in many respects. A shipboard version of the Su-27, with
canards, has been tested on Russia's first big carriers. It seems to go in
production. There also is a two-seat attack version, the SU-27IB, with
side-by-side seating in a reshaped nose.
Two 12500kg Lyulka AL-31F. 30mm gun. 10+ hardpoints for AA missiles. M2.35.
Analogous electrical remote control system.
Sold to China, India (Su-30MKI, tail No 56).
Traded to Bangladesh, Vietnam, S.Korea.
China will build Su-27SK under license.
Genealogy
- T-10-1 19.3K experimental prototype with AL-21F engines. >>>
- T-10S first serial version (AKA Su-27P or Su-27S) with AL-31F engines. >>>
- Su-27A 35.0K Flanker-A - (AL-31F) serial interceptor. no ground attack capabilities.
- Su-27S/T-10S - first serial interceptor for V.V.S. [OKB version of terms] (limited ground attack capabilities - free fall bombs, 100, 250, 500 kg caliber) >>>
- Su-27P - first srial air defense interceptors [TsAGI version of terms] (no ground attack capabilities)
- P-42 108.8K - record setting/experimental. unarmed. >>>
- Su-27P "Parrot painted" - two Su-27 and one Su-30 of LII aerobatic team lead by A.N.Kvochur. unarmed.
- Su-27PM - ?
- Su-27PMK - ?
- Su-27K/T-10K 47.0K - (naval, "Korabelnij") Carrier-fighter development >>>
- Su-27M - <27-Jun-1996>
The thrust vectoring Su-27M prototype is powered by AL-31FU engines that
vectors in pitch only. It's also fitted with a sidestick.
-- Urban Fredriksson.
- Su-35 (limited thrust vectoring AL-35F)
redesigned Su-27 with new engine, vectoring nozzles, radar, etc.
>>>
- Su-27LMK -
- Su-37 (AKA Su-27M2, full thrust vectoring AL-31FU, t/n 711) >>>
Since 2001[?] converted (and renamed) back to Su-35 by
removal of thrust-vectoring engines. It is now planned to be a series
production standard demonstrator ("etalon").
- Su-35UB - two-seater. >>>
- Su-27U
- Su-27UP
- Su-27UB 43.9K (two seat trainer/fighter/striker)
- Su-27UBK 32.2K - trainer
- Su-27PU - "mini AWACS"
- Su-27IB - really common name for a series of two-seaters.
- Su-27IB 34.4K -
AKA T-10V1, AKA Su-34-1, non-tandem main gear, t/n 42.
attack aircraft with side-by-side seating in a reshaped nose
- Su-32FN (tandem main gear, no rear radar, t/n 43 == T-10V-2) >>>
- Su-32FM (same a/c?, combat tests in Checnya in Jan'2000) >>>
- Su-34 AKA T-10V-3. tandem main gear, rear radar, t/n 43 (the T-10V-2), 44, and 45/349. >>>
- Su-30 - two-seat long range interceptor with aerial refuelling capability. (limited thrust vectoring) >>>
- Su-30PU - two-seat long range iterceptor >>>
- Su-30K - export version for China, Vietnam, and India. >>>
- Su-30MK - advanced export version >>>
- Su-30MKI (full thrust vectoring AL-31FU/AL-35F, export version for India) >>>
- Su-30 t/n 302 by Irkutsk IAPO. Anti-ship aircraft. Capable to use the P-900 Alpha (??) missile. Selected as the modernization prototype for serial Su-30 and Su-27 [sic!]. >>>
- Su-30KN joint development of t/n 302 and t/n 597 by Irkutsk IAPO. >>>
- Su-27UBK - export (Chinise) version.
- Su-27UBM - recce/strike version with high precision air-to-surface weapon. Tests have began 13-Jun-2001.
- Su-27SK licensed to China.
- J-11 Chinese...
Searchable map of Su-27 (not finished yet).
More: pic.1 8.3K, pic.2 42.2K, pic.3 19.3K, pic.4 122.3K, pic.5 81.4K, pic.6 66.5K, pic.7 56.6K, pic.8 86.5K, pic.9 80.2K, pic.10 73.1K, pic.11 16.3K, pic.12 90.3K, pic.13 15.6K, pic.14 9.8K, pic.15 20.6K, txt.16 [534], pic.17 25.5K, pic.18 35.0K, pic.19 34.4K, pic.20 47.0K, pic.21 9.9K, pic.22 42.5K, pic.23 43.9K, pic.24 32.2K, pic.25 27.3K, pic.26 69.4K, pic.27 22.6K, pic.28 53.9K, pic.29 618.9K, pic.30 685.4K, pic.31 115.1K, pic.32 171.9K, pic.33 38.3K, pic.34 130.2K, pic.35 137.5K, pic.36 273.2K, pic.37 41.5K, pic.38 181.0K, pic.39 57.7K, pic.40 69.4K, pic.41 27.4K, pic.42 26.1K, pic.43 22.6K, pic.44 72.4K, pic.45 48.2K, txt.46 [2.9K], pic.47 5.2K, pic.48 10.4K, aviapanorama.ru.
- Su-28 -
trainer/aerobatic/export version of Su-25.
Modification: Su-28 59.3K - trainer.
- Su-29 59.4K -
sports plane.
- Su-30 20.3K -
Two-seat long-range version of the Su-27 (formerly known as Su-27PU),
intended as long-range interceptor, 'Wild Weasel' aircraft and strike.
Production license was given to India.
More: pic.1 27.4K, pic.2 61.1K.
Stories: pic.1 1.2K pic.2 11.8K txt.3 [5.1K].
- Su-31 48.3K - aerobatic.
One M-14P engine.
Normal mass 832..882kg. Max takeoff mass 1100kg.
Modifications:
- Su-31M2 - "champion's" version.
with 400hp M-14PF engine, enlarged wing, 80kg less weight, new
ejectible seat SKS-94M, new cockpit.
- Su-32 [Designation reused!] -
newly selected name for modernized Su-27IB. tests will be finished by 2004..2005. NVO.
Primary trainer, replacing the Yak-52. Tandem-two seat aircraft with
retractable tricycle landing gear.
One 265kW Vedeneyev M-14P. 1996.
Early name of Su-34
Su-32FN 55.5K (latin "FN" for "Fighter Navi", name for Le-Bourget expo...).
Jet torpedoes of Su-32FN 56.8K.
Conventional torpedoes of Su-32FN 55.4K.
- Su-33 51.6K Flanker -
naval version of Su-27 (formerly Su-27K).
Carrier-fighter ("Korabelnij", so Su-27K) derivative of the Su-27, with canards
added, folding outer wing panels, strengthened undercarriage with twin
nosewheels, arrester hook. The use of thrust-vectoring nozzles on the production
aircraft is considered.
Entered service by the President Directive No1037, 31-Aug-1998.
Weapons 56.1K (Yakhont/Onyx missile on the front).
More: pic.1 47.2K.
- Su-34 16.4K/Su-32FN 50.7K/Su-27IB? -
Fighter-bomber replacement for the Su-24 Fencer. (formerly known as Su-27IB/KU)
Sukhoj designation for the Su-27IB, a two-seat ground-attack version of the
Su-27. The Su-27IB/Su-34 has side-by-side seating for two crewmembers in a
widened, flattened nose, with extended wing roots and canards, a larger tail
boom with rearward-looking radar, and twin-wheel landing gear. The VVS intends
to replace all Su-24s with the Su-34. Two Saturn 13300kg AL-31FM.
First flight 28-Dec-1994. First two were built at Novosibirsk Chkalov plant.
©«Indepedent Military Review» No21, 1997, p.6
Frontline fighter-bomber Su-34 was designed to attack aerial and
surface targets, including small and high speed targets, in the
tactical and operative depth of the enemy's order in day and night at
any weather conditions. The Su-34 is the deep modification of Su-27
fighter. Two twin-contoured afterbourning turbojets AL-31F (thrust of
12,800kg each) located in separate units under carrying fuselage.
It is possible to carry three extra fuel tanks of 3000l each.
The crew of two are the pilot and the navigator-operator seat side-by-side
in the armoured cockpit in ejectable seats K-36DM. Cockpit is entered via
the front gear bay.
On-board equipment includes a multifunction radar, optic-electronic
sight-and-observation system, readr sight radar, navigation equipment,
communication equipment, AEW. The equipment provides all means for the
following tasks (all weather, day and night): search, detection and
recognition of surface and aerial targets (including shipd, aircraft,
and missiles); generating data for sights, targeting and AEW systems;
automatic AA missiles targeting; group flight and co-operation;
generating technical, navigation, and tactical data for multifunction
pilot's screens.
The aircraft is equipped with builtin 30mm cannon GSh-301 (180
rounds), guided missiles and unguided rockets on 12 undercarriage
units. It can carry R-27(E) and RVV-AE mid-range missiles, short range
R-73, tactical short range AGMs X-25M and X-29, mid-range tactical
AGMs X-31P(A) and X-59M, guided bombs of 500kg and 1500kg caliber,
free fall bombs of 100kg to 500kg caliber, rockets of 80mm, 122mm,
and 266mm caliber.
The Su-34 was designed by Sukhoy OKB, in serial production since 1993
at Novosibirsk facility (APO named after V.P.Chkalov).
First flown 13-Apr-1990.
Aircraft: Su-34.
Take-off mass 39,000kg (max 45,100kg).
Combat load mass 8,000kg.
Fuel 12,100kg (with extra tanks 19,300kg).
Max speed at 11km 1,900km/h (at ground 1,400km/h).
Practical ceiling 15,000m.
Max overload 7.0.
Low altitude range 600km (with extra fuel tanks 1130km).
Max distance 4,500km.
Length 23.34m.
Wing span 14.7m.
Wing area 62.0m².
Heigth 6.36m.
See Su-27.
More: pic.1 17.7K, pic.2 36.1K, pic.3 29.3K, pic.4 67.5K, pic.5 9.0K, pic.6 56.8K, pic.7 48.3K, pic.8 239.4K, pic.9 45.4K, pic.10 31.7K, pic.11 31.1K, pic.12 65.7K, pic.13 118.2K, pic.14 16.2K.
A new designation for Su-25TM (???).
Story by Роман =KRoN= Каршиев in
FIDO RU.AVIATION:
|
Single wheel gear - Su-27IB (prototype, t/n ?42).
Twin-wheel gear - Su-32FN & Su-34.
Su-32FN are t/n 44 (s/n 343) and t/n 45 (s/n 349), while Su-34 - ?43.
Visual distinction is hard. I've seen too few Su-34s ;-)
The one i've seen had a radio-transparent fin of the tail boom
(perhaps, with a read-looking radar).
Su-32FN seems to have no rear-looking radar and carries a magnetic
mass detector instead.
|
С одиночным колесом - Су-27ИБ - прототип (борт ?42).
Су-32FN и Су-34 - со сдвоенными.
Су-32FN - борта 44 (343) и 45 (349), а Су-34 - ? 43.
Отличить их "на глаз" довольно сложно. Я слишком мало видел Су-34-х ;)
У того, что я видел - радиопрозрачная законцовка хвостовой балки - там
находится РЛС заднего обзора. Су-32FN таковой, кажется не имеет, вместо
неё встроен магнетометр.
|
Story by Alex Koval in
FIDO RU.AVIATION:
T-10V-1, the prototype of Su-34, (AKA Su-27IB, t/n 42) was built by
re-equipping of naval proto T-10-39 with vertical stabilizers from Su-27UB
(by another data: it was re-equipped from pre-production twin-seat trainer).
This was the cause of single-wheel gears.
Pre-serial aircraft ("product 66") by Novosibirsk APO are:
- T-10V-2 (t/n 43)
- T-10V-3 (t/n 45) - "exhibitional" ?349
- T-10V-4 (t/n 44) - "exhibitional" ?343
The last one can be T-10V-5 (and the 4-th used for static tests), or even
T-10V-3 as "t/n 43" and so on (and the 2-nd for static tests). I cannot
recall to be precise, in short. And more. Perhaps, there are two more Su-34.
|
Прототип самолета - Т-10В-1 (Су-27ИБ; борт 42) был получен переоборудованием
прототипа корабельной машины Т-10-39 с использованием килей от Су-27УБ (по
другим данным, переоборудован из предсерийной спарки). Отсюда - одноколесные
стойки шасси.
Предсерийные машины (изделие 66), выпущенные в Новосибирском АПО:
- Т-10В-2 (борт 43)
- Т-10В-3 (борт 45) - "выставочный" ?349
- Т-10В-4 (борт 44) - "выставочный" ?343
Последний, может быть Т-10В-5 (а 4-й построен для статиспытаний), или даже
так: Т-10В-3 - борт 43 и т. д. (а 2-й - для статиспытаний). Короче, точно не
помню. И еще. Вроде в Новосибе в некоторой степени готовности находятся еще
пара Су-34.
|
Story by Vladimir Malukh in
FIDO RU.AVIATION:
t/n 42 - AKA Su-27IB, the very first proto of strike a/c T-10B-1.
It was built on the base of standard twin-seater with just another
head. The construction of the "real" Su-34 was changed more deeply
after the tests of T-10B-1.
34 and 32FN differ visually by form and painting of tail fin.
34 has a radio-transparent white fin, while 32FN has a magnetically
transparent camouflaged fin.
There should be 12 aircraft to be assembled to 1998, but due to
obvious reasons (no money) the assembly programm failed. Three were
assembled for sure and they are flying, including t/n 44 (s/n 343),
anyway, i have photos of them all. The t/n 45 is the FN (s/n 349).
|
Борт 42 - это то что называли Су-27ИБ, те самый первый прототип
ударного самолета T-10Б-1. Его сделали на базе стандартной спарки,
заменив лишь носовую часть фюзеляжа. Конструкция "настоящего" Су-34
изменена более существенно по результатам испытаний Т-10Б-1.
34 и 32ФН различаются внешне по форме и окраске хвостового обтекателя
- У 34 он радиопрозрачный и как правило белый, у 32ФН наоборот он так
сказать магнитопрозрачный (дюралевый тк. легче пластика) и окрашен в
тот же камуфляж что и сам самолет.
К 98 году должно было быть собрано 12 машин, но из-за очевидных причин
(нет денег) программа сборки сорвана - три собрали точно, и они
летают, в том числе и борт 44 (второй номер 343), во всяком случае у
меня есть фотографии их всех. Модификацией ФН кажется является борт 45
(второй номер 349)
|
- Su-35 18.0K -
Improved 'glass cockpit' version of the Su-27, with canard foreplanes, more
powerful radar, more powerful engines, and possibly thrust-vectoring nozzles,
and an electronics upgrade. The first aircraft able to make Mach 1.0+... in
vertical flight. (first one: t/n 709?).
MTOW 45t (8t of weapons). Digital FBW.
Two 137.3kN Saturn-Lyulka AL-31MF (the vectored thrust is the AL-35FM).
First flown May, 1985.
-
Once the a/c was landed without the assistance of onboard computer!
Test pilot Oleg Grigorievitch Tsoy could fly over 150km and land safely the almost
uncontrolled aircraft with ~500kg real bomb on the undercarriage...
Colonell O.Tsoy became the Hero of Russia.
Modifications:
- Su-35UB - two seats combat/trainer.
More: pic.1 92.3K, pic.2 18.0K pic.3 61.9K pic.4 59.3K, pic.5 59.5K, pic.6 54.9K.
- Su-37 36.1K (AKA Su-27M2) -
Proposed multi-role combat aircraft with foreplanes, vectored thrust engines,
and super-maneurability features.
Digital electrical remote control system.
Two AL-31FP engines (1000 hours) with
trust vectoring nozzles (250 hours, maybe rlolonged to 500 hours).
Max speed 2500km/h. 14 (another data: 12) undercarriages.
(first one: t/n 711, converted to Su-35 state (see also))
More: pic.1 155.3K, pic.2 19.6K, pic.3 19.3K, pic.4 22.1K, txt.5 [1.3K], pic.6 7.9K, pic.7 37.1K, pic.8 33.4K, pic.9 36.1K, pic.10 38.2K, pic.11 30.7K.
- Su-38 - single seat agricultural.
One 360hp M-14P engine.
Length 7.63m. Heigth 2.3m. Wing span 11.15m. Weight 1050..2100kg.
Original data was found here.
Modifications:
- Su-38L - agricultural.
400..600kg of chemical load.
Test flight planned for spring 2001.
5 aircrafts to be built and sertified by end of 2001.
Estimated price USD120..130K.
Estimated market 500 units.
- Su-39 7.8K -
anti-tank version of Su-25.
A story from Military Parade
Su-39 was incorrectly reported here as a trainer version of Su-26/Su-32.
Date: Thu, 19 Jun 1997 11:29:51 +0000
From: Marian Miller
Subject: Su-39
Hi !
I think, I found a mistake.
I've recently seen a Su-39 propagation picture and it had no similarity
to Su-26.
It is a development of Su-25 with better avionics, armament and
a new defense system including new ECM jammers and automatic flare
dispensers. It also has the K-36 Zvezda rescue system.
It should have a new 30-mm revolver cannon instead of the GSh-30 twin.
Please, send me mail, whether I am right or not.
28-Jun-1999 the story got the continuation!
Alexandre Savine, master of RAM,
pointed me an article,
describing the aircraft:
-
Two seat primary trainer.
400hp M-14PF engines planned, but more reliable 360hp M-14P used.
Takeoff weight 1300kg. Empty weight 850kg.
Speeds, km/h: max 370, landing 110. Climb rate 13.5m/s.
Max allowed overload +11/-8.
Range 1500km. Take off run 230m. Landing run 350m.
Ceiling 7000m. Life time 10000 hours.
First flight planned to 2001.
Based on S-26 and Su-29.
Plus, at Gustin's page we read:
-
Year: 1996 Crew: 2 Engines: 1 * 300kW Vedeneyev M-14PF
Wing Span: 8.50m Length: 7.28m Height: 2.60m Wing Area: 12.20m2
Empty Weight: 850kg Max.Weight:
Speed: 370km/h Ceiling: 7000m Range: 1500km.
More: pic.1 55.6K.
- Su-47 159.8K -
new name of S-37 since MACS'2001 air show.
See MACS'2001 for much more pics.
- Su-49 - a trainer.
02-Oct-2002 -- entering serial production at NAPO.
Su-trainers genealogy:
- Su-26
- Su-29, two seater
- Su-49???
- Su-80 -
"new name" for S-80 invented by media.
The name aquired by producers.
4 flying aircrafst were built by KnAAPO for Border Guards and
Forset Service.
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