Cockpit

Refuelling probe

               History

The need to replace outdated S-2 fighters was obvious in the early 1970s. The team of engineers of the Vinnytsia Aviation Design Bureau received an order to create a supersonic fighter for Air Force.
In 1974, the development of a new fighter began and continued until the fall of 1981. In the same year, a model of the plane was made. In the summer of 1983, an experimental model of the aircraft was made, and tests were conducted in the fall of the same year.
With a creak, the plane passed the test and V.A. received an order for a series of 50 aircraft, but only 32 was built.

    Performance characteristics 

Run length: 920m
Takeoff speed: ~385kph
Maximum speed at 500m: ~1350kph
Maximum speed at 8km: ~1800kph
Do not exceed speed 450m/s.

    Weapons

PM-5 — Short-range air-to-air missile
max range — 5km
Max speed — 620m/s

PC-20 — Medium-range air-to-air missile
Max range — 20km
Max speed — 1000m/s

HEB-250 — 250kg bomb

Unnamed — rocket pod(8 rockets)

    Control

Ag1 — canopy;
Ag3 — refuelling probe;
Ag4 — navigation lights;
Ag5 — air brake;
Ag6 — parachute;
Ag7 — Electronics in the cockpit;
Ag8 — engine;
Throttle 100% — afterburner.

P.S.

Hud — PlanariaLab;
Radar — Zaineman.