Additional information
| Base chassis | Tracked self-propelled steam |
|---|---|
| Engine | Turbojet ВК-1 А |
| Quantity of engines | 2 |
| Engine thrust, kg | 1920 |
| nominal rotational speed, RPM | 9000 |
| Maximum number of turns, RPM | 10000 |
| The amount of exhaust gases, with n = 9000 rpm (for one engine), kg / s | 38 |
| м | 645 |
| Fuel consumption at n = 9000 rpm - for one engine, l / (kgtyag.ch) | 1,6 |
| Hourly fuel consumption, kg / h (l / h) | 1472 (1840) |
| Fuel tank capacity, l, not less | 2500 |
| Turbo-jet installation capacity, kg / s, not less | 200 |
| Water supply, m3 (l) | 120 |
| Lifting angle of a turbojet unit, degrees, not less | up 60, down 15 |
| horizontal rotation angle | 180 |
| Water consumption for protection from radiant heat, l / s | 20 |
| Overall dimensions (length: width: height), mm | 9000:3500:3500 |
| The number of places for combat crew, people | 3 |
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