Parameters
The maximum take-off thrust is 70 kGs
Specific fuel consumption (at maximum thrust) is 1.14 kg / hgf h
Output electric power - 1100 W
Start-up system - electric starter
Fuel system - electric fuel pump
Lubrication system - oil circulating
Mean time between failures - 3000 h
The assigned service life is 1000 h or 15 years or 1800 starts
Inter service interval - 200 h or 2 years or 300 starts
Resource before overhaul - 400 h or 8 years or 800 starts
Maximum continuous operation time - 2 h
Overall dimensions - diameter 367 mm, length 485 mm

Fuel
Aviation kerosene