In numbers Through the lens Video
In the 1950's the Miasitsev design Office (OKB-23), had developed a series of nuclear-powered bombers. To protect the crew, an armored cockpit was proposed (the weight of the armor exceeded 38.000 kg). The bomber designs were ready in May 1950.
Three-view drawing
.jpg "M-30 © Konstantinos Panitsidis")
Technical specifications
| DESIGNER | OKB-23 (V.M. Myasishchev) |
| COUNTRY | Russia |
| TYPE |
Project strategic bomber
|
| CREW | 2 |
| POWER-PLANT | Nuclear power plant, RD-A |
| Thrust, kgf | |
| DIMENSIONS | |
| Length, m | - |
| Height, m | - |
| Wing span, m | - |
| Wing area, m2 | - |
| Wing sweep angle, degree | - |
| WEIGHT | |
| Maximum take-off, kg | 169.000 - 170.000 |
| Normal take-off, kg | - |
| Empty aircraft, kg | - |
| Internal fuel, l | - |
| Warload, kg | up to 25.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 1.350 |
| Cruising speed, km/h | - |
| Practical ceiling, m | 18.000 |
| Range, km | 8.000 |
| Combat range, km | |
| ARMAMENT |
Missile and bombs of various types, depending on the type of mission it performs.
|