.jpg "Glushenkov TVD-10B Turboprop engine © Konstantinos Panitsidis")
In numbers Through the lens Video
Technical specifications
| DESIGNER | Glushenkov |
| COUNTRY | Russia |
| TYPE |
Turboprop engine
|
| Installed On (aerial means) |
An-28, PZL M28
|
| Fuel | T-1, T-2, TS-1, Jet A-1 |
| Oil | - |
| Propeller shaft power, take-off power rating | 960 h.p. |
| Specific fuel consumption, take-off power rating | 0,255 kg/h.p.*h |
| Propeller shaft power, cruise power | 510 h.p |
| Specific fuel consumption, cruise power | 0,335 kg/h.p.*h |
| Pressure ratio, take-take-off power rating | 7,4 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.160 K |
| Air flow rate, take-off power rating | 4,58 kg/sec |
| OVERALL DIMENSIONS | |
| Diameter | - |
| Height | 900 mm |
| Width | 555 mm |
| Length | 2060 mm |
| WEIGHT | |
| Engine weight | 225 kg |
| Specified service life | - |