Sojuz R179-300
200,1 kN x 101,97 kg/kN / 0,454 kg/lb = 44 943.165 lb of thrust
It seems that this engine wanished from their web :-\ http://www.amntksoyuz.ru/en/engines/airengines/history/
But I saved everything to my archive...

But currently I dont have access to it because the malfunction of my computer :

But I can use my web ;D
Thrust: 200,1 kN
Weight: 2880 kg
Diameter 1,75 m
Lenght: 5,61 m
Fuel consumption: 0,064 kg/N/h
Air consumption: 180 kg/s
In/out air pressure ratio: 25
Bypass ratio: 0,73