In Czechoslovakia the sa was considered with the use of this engineand on the drive lietadla let L-610 pre zahraničie (the traditional trhoch sa was considered with motorom M-602).
Dĺžka - 2438 mm
Max. priemer engineand - 737 mm
Hmotnosť empty engineand - 360,6 kg
Kompresný ratio - 18:1
Take-off power - 1305 kW
Max. take-off power - 1395 kW
Max. cost performance vo výške 4575 m - 1052 kW
Source:
Sara Said, Jan F.: The chances of success, the Aviation and aerospace 1990 / 10.
Dĺžka - 2438 mm
Max. priemer engineand - 737 mm
Hmotnosť empty engineand - 360,6 kg
Kompresný ratio - 18:1
Take-off power - 1305 kW
Max. take-off power - 1395 kW
Max. cost performance vo výške 4575 m - 1052 kW
Source:
Sara Said, Jan F.: The chances of success, the Aviation and aerospace 1990 / 10.