Search results
Results from the WOW.Com Content Network
Illustration of Yakovlev Yak-141 The wing was mounted high on the fuselage, and was foldable to allow for compact storage on board aircraft carriers . The main engine was a Tumansky R-79V-300 , while the lift jets were a pair of Rybinsk (RKBM) RD-41s , installed at an angle of 85° in the forwards fuselage behind the cockpit.
The bureau formed in 1934 under aircraft designer Alexander Sergeyevich Yakovlev as OKB-115 (the design bureau has its own production base at the facility No.115), but dates its birth from 12 May 1927, the day of maiden flight of the AIR-1 aircraft developed within [citation needed] the Department of Light Aircraft of GUAP (Head Agency of Aviation Industry) under the supervision of A.S. Yakovlev.
Yak-100/Yak-22 (1948 - projected transport helicopter design, initially named as Yak-22) Yak-140 (1954 - experimental fighter aircraft; cancelled in favor of the MiG-21) Yak-141/Yak-41 "Freestyle" (1987 - prototype supersonic VTOL fighter, initially named as Yak-41) Yak-201 (Fifth-generation VTOL aircraft intended for the Russian Navy in the ...
The Yakovlev Yak-201 was a planned Russian vertical takeoff and landing stealth fighter/interceptor aircraft for the Russian Navy, as a follow-up to the Yak-141 and Yak-43 aircraft. [1] The design was carried out in the mid-1990s Yakovlev Design Bureau . [ 2 ]
The Yakovlev Yak-130 (NATO reporting name: Mitten) [3] is a subsonic two-seat advanced jet trainer and light combat aircraft originally developed by Yakovlev and Aermacchi as the "Yak/AEM-130". It has also been marketed as a potential light attack aircraft.
The only mistake is to apply it to all Yak-41s. I think your addition to the "variants" section sums it up nicely; although I do question the use of the word "fictitious". --Rlandmann 11:15, 17 February 2010 (UTC) Moves should be discussed beforehand. The Yak-141 designation issues seemed to be already covered in the "Yak-41 or Yak-41?"
The Yak-140 was developed around the Mikulin AM-11 turbojet (rated at 40 kN (9,000 lb f) thrust dry and 50 kN (11,000 lb f) with afterburner) to meet a specification issued in 1953 requiring a supersonic fighter with a maximum speed of 1,650–1,750 km/h (1,030–1,090 mph) and a range of 1,800 km (1,100 mi). It was to be armed with three 30 mm ...
Yakovlev Yak-141; Yakovlev Yak-200; ... Yakovlev Yak-201 This page was last edited on 23 June 2022, at 14:26 (UTC). Text is available under the Creative ...