In numbers Through the lens Video
Αlso known as: Yak-XX or Yak-201
VTOL - vertical take-off and landing
V/STOL - A vertical and/or short take-off and landing
The "Yakovlev" design office at one point proposed its own design for a 5th generation fighter aircraft. His proposal was for a single-engine aircraft, with a triangular wing, tailless and at front canards.
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| Another 5th generation light fighter design. As published in a book by Yefim Gordon entitled "Russian Experimental Fighters of New Generation MFI and S-37", published by Polygon 2001. The aircraft was intended to be fitted with a thrust-deflection variable nozzle propulsion system and an RD-33 lift engine, specially modified for nose mounting in front of the cockpit. The design of the new "Yak-XX or Yak-201" included almost all the features of a stealth technology aircraft. |
Technical specifications
| DESIGNER | OKB Yakovlev |
| COUNTRY | Russia |
| TYPE |
A vertical and, or short take-off and landing, stealth technology.
|
| CREW | 1 |
| POWER-PLANT | One turbofan engine AL-41F and possibly an RD-33 type engine |
| Thrust, kgf | |
| - with afterburning | 1x20.000 |
| - without afterburner | 1x12.500 |
| Engine lift | RD-33 |
| Thrust, kgf | 1x5.040 |
| DIMENSIONS | |
| Length, m |
18,80
|
| Height, m |
-
|
| Wing span, m |
11,70
|
| Wing area, m2 |
42,00
|
| WEIGHT | |
| Maximum take-off, kg | 25.800 |
| Normal take-off, kg | 20.000 |
| Empty aircraft, kg | 15.300 |
| Internal fuel, kg | 6.500 |
| Warload, kg | 4.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.100 |
| Cruising speed, km/h | - |
| Maximum speed in low height, km/h | - |
|
Rate of climb, m/s
|
- |
| Service ceiling, m | - |
| Range, km | 4.000 |
| Combat range, km | - |
| Maximum overload, g | - |
| ARMAMENT | Doesn't have (defensive). |
| Note | Specifications estimated |