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| <!-- This article is a part of ]. Please see ] for recommended layout. --> | |||
| {|{{Infobox aircraft begin | |||
| | name= | |||
| | image= | |||
| | caption= | |||
| }}{{Infobox aircraft type | |||
| | type= | |||
| | national origin= | |||
| | manufacturer= | |||
| | designer= | |||
| | first flight= | |||
| | introduced= | |||
| | retired= | |||
| | status= | |||
| | primary user= | |||
| | more users= <!--Limited to three in total; separate using <br /> --> | |||
| | produced= <!--years in production--> | |||
| | number built= | |||
| | program cost= <!--Total program cost--> | |||
| | unit cost= <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> | |||
| | developed from= | |||
| | variants with their own articles= | |||
| }} | |||
| |} | |||
| <!-- ==Development== --> | |||
| <!-- ==Design== may be combined with above as "Design and development" --> | |||
| <!-- ==Operational history== --> | |||
| <!-- ==Variants== --> | |||
| <!-- ==Units using this aircraft/Operators (choose)== --> | |||
| ==Specifications (variant specified) == | |||
| {{Aircraft specs | |||
| |ref=<!-- reference --> | |||
| |prime units?=<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, | |||
| met(ric) first for all others. You MUST choose a format, or no specifications will show --> | |||
| <!-- | |||
| General characteristics | |||
| --> | |||
| |genhide= | |||
| |crew= | |||
| |capacity= | |||
| |length m= | |||
| |length ft= | |||
| |length in= | |||
| |length note= | |||
| |span m= | |||
| |span ft= | |||
| |span in= | |||
| |span note= | |||
| |upper span m= | |||
| |upper span ft= | |||
| |upper span in= | |||
| |upper span note= | |||
| |mid span m= | |||
| |mid span ft= | |||
| |mid span in= | |||
| |mid span note= | |||
| |lower span m= | |||
| |lower span ft= | |||
| |lower span in= | |||
| |lower span note= | |||
| |swept m=<!-- swing-wings --> | |||
| |swept ft=<!-- swing-wings --> | |||
| |swept in=<!-- swing-wings --> | |||
| |swept note= | |||
| |dia m=<!-- airships etc --> | |||
| |dia ft=<!-- airships etc --> | |||
| |dia in=<!-- airships etc --> | |||
| |dia note= | |||
| |width m=<!-- if applicable --> | |||
| |width ft=<!-- if applicable --> | |||
| |width in=<!-- if applicable --> | |||
| |width note= | |||
| |height m= | |||
| |height ft= | |||
| |height in= | |||
| |height note= | |||
| |wing area sqm= | |||
| |wing area sqft= | |||
| |wing area note= | |||
| |swept area sqm=<!-- swing-wings --> | |||
| |swept area sqft=<!-- swing-wings --> | |||
| |swept area note= | |||
| |volume m3=<!-- lighter-than-air --> | |||
| |volume ft3=<!-- lighter-than-air --> | |||
| |volume note= | |||
| |aspect ratio=<!-- sailplanes --> | |||
| |airfoil= | |||
| |empty weight kg= | |||
| |empty weight lb= | |||
| |empty weight note= | |||
| |gross weight kg= | |||
| |gross weight lb= | |||
| |gross weight note= | |||
| |max takeoff weight kg= | |||
| |max takeoff weight lb= | |||
| |max takeoff weight note= | |||
| |fuel capacity= | |||
| |lift kg=<!-- lighter-than-air --> | |||
| |lift lb=<!-- lighter-than-air --> | |||
| |lift note= | |||
| |more general= | |||
| <!-- | |||
| Powerplant | |||
| --> | |||
| |eng1 number= | |||
| |eng1 name= | |||
| |eng1 type= | |||
| |eng1 kw=<!-- prop engines --> | |||
| |eng1 hp=<!-- prop engines --> | |||
| |eng1 shp=<!-- prop engines --> | |||
| |eng1 kn=<!-- jet/rocket engines --> | |||
| |eng1 lbf=<!-- jet/rocket engines --> | |||
| |eng1 note= | |||
| |power original= | |||
| |thrust original= | |||
| |eng1 kn-ab=<!-- afterburners --> | |||
| |eng1 lbf-ab=<!-- afterburners --> | |||
| |eng2 number= | |||
| |eng2 name= | |||
| |eng2 type= | |||
| |eng2 kw=<!-- prop engines --> | |||
| |eng2 hp=<!-- prop engines --> | |||
| |eng2 shp=<!-- prop engines --> | |||
| |eng2 kn=<!-- jet/rocket engines --> | |||
| |eng2 lbf=<!-- jet/rocket engines --> | |||
| |eng2 note= | |||
| |eng2 kn-ab=<!-- afterburners --> | |||
| |eng2 lbf-ab=<!-- afterburners --> | |||
| |eng3 number= | |||
| |eng3 name= | |||
| |eng3 type= | |||
| |eng3 kw=<!-- prop engines --> | |||
| |eng3 hp=<!-- prop engines --> | |||
| |eng3 shp=<!-- prop engines --> | |||
| |eng3 kn=<!-- jet/rocket engines --> | |||
| |eng3 lbf=<!-- jet/rocket engines --> | |||
| |eng3 note= | |||
| |eng3 kn-ab=<!-- afterburners --> | |||
| |eng3 lbf-ab=<!-- afterburners --> | |||
| |more power= | |||
| |prop blade number=<!-- propeller aircraft --> | |||
| |prop name= | |||
| |prop dia m=<!-- propeller aircraft --> | |||
| |prop dia ft=<!-- propeller aircraft --> | |||
| |prop dia in=<!-- propeller aircraft --> | |||
| |prop dia note= | |||
| |rot number=<!-- helicopters --> | |||
| |rot dia m=<!-- helicopters --> | |||
| |rot dia ft=<!-- helicopters --> | |||
| |rot dia in=<!-- helicopters --> | |||
| |rot area sqm=<!-- helicopters --> | |||
| |rot area sqft=<!-- helicopters --> | |||
| |rot area note= | |||
| <!-- | |||
| Performance | |||
| --> | |||
| |perfhide= | |||
| |max speed kmh= | |||
| |max speed mph= | |||
| |max speed kts= | |||
| |max speed note= | |||
| |max speed mach=<!-- supersonic aircraft --> | |||
| |cruise speed kmh= | |||
| |cruise speed mph= | |||
| |cruise speed kts= | |||
| |cruise speed note= | |||
| |stall speed kmh= | |||
| |stall speed mph= | |||
| |stall speed kts= | |||
| |stall speed note= | |||
| |never exceed speed kmh= | |||
| |never exceed speed mph= | |||
| |never exceed speed kts= | |||
| |never exceed speed note= | |||
| |minimum control speed kmh= | |||
| |minimum control speed mph= | |||
| |minimum control speed kts= | |||
| |minimum control speed note= | |||
| |range km= | |||
| |range miles= | |||
| |range nmi= | |||
| |range note= | |||
| |combat range km= | |||
| |combat range miles= | |||
| |combat range nmi= | |||
| |combat range note= | |||
| |ferry range km= | |||
| |ferry range miles= | |||
| |ferry range nmi= | |||
| |ferry range note= | |||
| |endurance=<!-- if range unknown --> | |||
| |ceiling m= | |||
| |ceiling ft= | |||
| |ceiling note= | |||
| |g limits=<!-- aerobatic --> | |||
| |roll rate=<!-- aerobatic --> | |||
| |glide ratio=<!-- sailplanes --> | |||
| |climb rate ms= | |||
| |climb rate ftmin= | |||
| |climb rate note= | |||
| |time to altitude= | |||
| |sink rate ms=<!-- sailplanes --> | |||
| |sink rate ftmin=<!-- sailplanes --> | |||
| |sink rate note= | |||
| |lift to drag= | |||
| |wing loading kg/m2= | |||
| |wing loading lb/sqft= | |||
| |wing loading note= | |||
| |disk loading kg/m2= | |||
| |disk loading lb/sqft= | |||
| |disk loading note= | |||
| |fuel consumption kg/km= | |||
| |fuel consumption lb/mi= | |||
| |power/mass= | |||
| |thrust/weight= | |||
| |more performance= | |||
| <!-- | |||
| Armament | |||
| --> | |||
| |armament=<!-- add bulletted list here or if you want to use the following | |||
| specific parameters, remove this parameter--> | |||
| |guns= | |||
| |bombs= | |||
| |rockets= | |||
| |missiles= | |||
| |hardpoints= | |||
| |hardpoint capacity= | |||
| |hardpoint rockets= | |||
| |hardpoint missiles= | |||
| |hardpoint bombs= | |||
| |hardpoint other= | |||
| |avionics= | |||
| }} | |||
| ==References== | |||
| {{reflist}} | |||
| <!-- ==Further reading== --> | |||
| <!-- ==External links== --> | |||
| <!-- Navboxes go here --> | |||
| ] | |||
| Work on creating an attack aircraft to replace ] was started in 1984. The first project was ready by 1989. The theme was called Sturmovik-90. One of the options developed in Sukhoi Design Bureau received the T-12 index. It was a very unusual car. The plane had a carrying body with two cabins between which the channels ] s were located, with ]s. At their ends were placed containers with EW equipment. In the left cockpit there was a pilot and under the radio transparent ] there was a radar, and in the right cockpit ] was located and under the fairing there was an optical-electronic system. | Work on creating an attack aircraft to replace ] was started in 1984. The first project was ready by 1989. The theme was called Sturmovik-90. One of the options developed in Sukhoi Design Bureau received the T-12 index. It was a very unusual car. The plane had a carrying body with two cabins between which the channels ] s were located, with ]s. At their ends were placed containers with EW equipment. In the left cockpit there was a pilot and under the radio transparent ] there was a radar, and in the right cockpit ] was located and under the fairing there was an optical-electronic system. | ||
Revision as of 04:36, 3 January 2019
| Role | Type of aircraft |
|---|---|
Specifications (variant specified)
General characteristics Performance
References
]
Work on creating an attack aircraft to replace Su-25 was started in 1984. The first project was ready by 1989. The theme was called Sturmovik-90. One of the options developed in Sukhoi Design Bureau received the T-12 index. It was a very unusual car. The plane had a carrying body with two cabins between which the channels air intake s were located, with forward-swept wings. At their ends were placed containers with EW equipment. In the left cockpit there was a pilot and under the radio transparent fairing there was a radar, and in the right cockpit Weapon Operator was located and under the fairing there was an optical-electronic system.
Weapons
Armament is mainly located in two internal compartments. Although it was possible to place additional weapons on the underwing pylons. Work on the T-12 took place at a very serious pace and the assembly line at the plant in Irkutsk was being prepared, but the events of the nineties put an end to this project.
Flight performance
Estimated take-off weight was about 20 tons, engine thrust (both single- and twin-engine variants were considered) —about 100 kN. The length of the aircraft - 16 m, wingspan - 19.5 m. Fuel capacity - 4500 kg, combat load - 6500 kg. Maximum speed - 1000 km / h, cruising - 835 km / h.
See also
Links
| Sukhoi aircraft | |
|---|---|
| Fighters / interceptors | |
| Bombers / attack | |
| Reconnaissance | |
| Competitive aerobatic | |
| Trainers | |
| Transports | |
| Experimental | |
| Agricultural | |
| Cancelled projects | |
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