In numbers Through the lens Video
Developed by the design office OKB-23, headed by V.M. Myasischev in 1960 and concerned a tailless aircraft. Only some models were developed.
The entire program was terminated when the OKB-23 merged with the OKB-52, headed by V.A. Tchelomey.
Three-view drawing
Technical specifications
| DESIGNER | OKB-23 (V.M. Myasishchev, G.N.Nazarov) |
| COUNTRY | Russia |
| TYPE |
Heavy supersonic bomber
|
| CREW | 2 (4-5) |
| POWER-PLANT | Six turbojet engines VK-15M |
| Thrust, kgf | |
| - with afterburning | 6x15.800 |
| - without afterburner | 6x10.000 |
| DIMENSIONS | |
| Length, m | 62,45 |
| Height, m | - |
| Wing span, m | 32,00 |
| Wing area, m2 | - |
| Wing sweep angle, degree | - |
| WEIGHT | |
| Maximum take-off, kg | 200.000 |
| Normal take-off, kg | - |
| Empty aircraft, kg | - |
| Internal fuel, l | - |
| Warload, kg | |
| - standard configuration | 5.000 - 9.000 |
| - maximum | 20.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.000 |
| Cruising speed, km/h | - |
| Maximum speed in low height, km/h | - |
| Service ceiling, m | 18.000 |
| Range, km | 10.000 |
| Combat range, km | - |
| ARMAMENT |
Bombs - up to FAB-5000, two X-22 shells (Kh-22) or two "44" missiles.
|