soloviev d-30 thrust：Thrust
About
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The Soloviev D-30 (now the Aviadvigatel PS-30) is a Soviet two-shaft low-bypass turbofan engine, officially referred to as a bypass turbojet.
D
https://www.polot.net
The thrust at the cruising altitude of 11,000 m at Ma-0.8 is 14.22 kN (1,450 kG). The temperature in front of the turbine is 1,316 degrees C.
Soloviev D
https://en.wikipedia.org
In 1980, the D-30 engine series III, a further improvement, was created with the maximum thrust of 6930 kgf (with preserving it at up to до = +C). The ...
Soloviev D
http://www.tmkb-soyuz.ru
Soloviev D-30 aircraft engine is two-shaft turbofan engine with integrated ... Thrust, kgf – 9500. Specific fuel consumption, kg/kgf hour – 0,72. Full ...
Soloviev D
https://www.redstar.gr
Max thrust take-off power rating, 11.000 kgf. Specific fuel consumption, take-off power rating, 0,49 kg/kgf.*h. Max thrust, cruise power, 2.750 kgf. Specific ...
Soloviev D
https://www.aircraftinvestigat
performance calculations for the Soloviev D-30KU aircraft engine. Soloviev D-30KU turbofan engine of 112.8 [KN] (25358 [lbf]) thrust.
What is the most powerful military jet engine?
https://militaryaircraft.quora
In terms of thrust I believe it is the Rolls Royce Trent 774 on the KC-30 / A330 derived Tankers. I am not aware of a more powerful turbofan in ...