Revision as of 22:05, 3 January 2019 editBoleyn (talk | contribs)Autopatrolled, Extended confirmed users, Page movers, New page reviewers, Pending changes reviewers307,295 edits Added tags to the page using Page Curation (unreferenced)← Previous edit | Revision as of 20:20, 6 January 2019 edit undoArado (talk | contribs)Extended confirmed users42,616 editsNo edit summaryNext edit → | ||
Line 251: | Line 251: | ||
<!-- Navboxes go here --> | <!-- Navboxes go here --> | ||
] | |||
Revision as of 20:20, 6 January 2019
This article does not cite any sources. Please help improve this article by adding citations to reliable sources. Unsourced material may be challenged and removed. Find sources: "Sukhoi T-12 Shturmovik-90" – news · newspapers · books · scholar · JSTOR (January 2019) (Learn how and when to remove this message) |
Role | Ground attack aircraftType of aircraft |
---|---|
National origin | Soviet Union |
First flight | not flown |
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 | |
This article on a bomber aircraft is a stub. You can help Misplaced Pages by expanding it. |