Yakovlev Yak-201
| Industry | Aerospace |
|---|---|
| Headquarters | Russia |
| Products | Aircraft designs, including Yak-201 VTOL fighter project |
The Yakovlev Yak-201 represented a proposed Russian vertical takeoff and landing (VTOL) stealth fighter/interceptor intended for deployment by the Russian Navy. It was conceived as a successor to the earlier Yak-141 and Yak-43 models. The Yakovlev Design Bureau undertook the design process during the mid-1990s. However, the initiative was ultimately discontinued without any prototype construction, primarily due to insufficient funding and waning interest from the Russian Ministry of Defense.
Development
In the mid-1990s, the Yakovlev bureau independently initiated the design of a modern VTOL aircraft tailored to operate from Russian naval aircraft carriers, aiming to enhance carrier-based aviation capabilities. Following the development of the Yak-141 and Yak-43, Yakovlev engineers advanced their work towards creating the Yak-201.
Between 1996 and 1997, the Yak-201 was presented to potential users, but it failed to secure orders. The main obstacles included financial constraints and uncertainty within the Russian Ministry of Defense regarding commitments under the LFI program. Consequently, no full-scale mock-ups or prototypes were produced.
On 23 November 2017, reports indicated that Yakovlev had been selected to design a new VTOL aircraft intended for operation aboard future Russian aircraft carriers, such as those envisioned in the Project 23000 aircraft carrier#Project 2300 Shtorm or Project 11430E Lamantin proposals. While it remains unclear if this new design would derive from the Yak-201, Yakovlev might develop a fresh VTOL fighter for deployment on the two 44,000-ton Project 23900 amphibious assault ship#Project 23900 Ivan Rogov amphibious assault ships currently being constructed.
Design
This aircraft was intended to distinguish itself from the Yak-141 and Yak-43 through enhanced range, a single-engine configuration, and stealth features. It follows a conventional layout with twin vertical stabilizers set at a steep angle. The design emphasizes reduced radar visibility by minimizing sharp angles, contributing to its relative stealthiness. Preliminary information from the design bureau indicates the interceptor fighter was planned to accommodate only one pilot.
The concept involved a single lift-propulsion engine mechanically linked to a lift fan positioned behind the cockpit. The main engine's exhaust nozzle was designed to be vectorable, with considerations for both flat and round nozzle shapes. This thrust vectoring capability would grant the aircraft exceptional maneuverability. Weaponry was intended to be housed within an internal bay located in the fuselage.
Performance targets included a maximum speed of 1,250 km/h at low altitude and up to 1,800 km/h at higher altitudes. The operational ceiling was projected to reach 15,000 meters. Armaments were planned to feature a GSh-301 cannon loaded with 120 rounds, alongside air-to-air missiles such as the R-77 for long or medium-range engagements, mounted on four external hardpoints. Integration of short-range missiles like the R-73, R-60, and unguided rockets up to 240 mm caliber was also explored.