It's thrust is 27,300 lbs per engine.
This information should be available on the Boeing website or other avaition-related websites. For a quick answer, I will related my experiences from 1970's. Boeing certified the B747-200 to operate with General Electric CF6-50 engines. During take-off power, each GE engine could produce 56,000 lbs of thrust per enginer: or 224,000 lbs for a few minutes. Now, the larger B747-400 a/c have more powerful engines. Currently each engine on a Boeing 747-400 can generate a maximum of about 63,300 lbs of thrust. Accordingly, since this aircraft has four engines it can produce total thrust of about 253,000 lbs.
A Boeing 747 typically produces between 66,500 to 70,000 pounds of thrust per engine, depending on the specific model and engine type. With four engines, the total thrust can range from approximately 266,000 to 280,000 pounds. This thrust is essential for the aircraft's performance during takeoff and climbing phases.
A Boeing 747 typically has four engines, and each engine produces approximately 66,500 to 70,000 pounds of thrust, depending on the specific model and engine type. This means the total thrust generated by all four engines can range from about 266,000 to 280,000 pounds. The high thrust allows the aircraft to efficiently take off and climb at high altitudes.
For the (Next Generation) Boeing 737 family, the most powerful engine powerplant avaliable for it (the CFM 56-7B27) produces 27,300 lbf (121.4 kN) of thrust.
The power required for takeoff of a Boeing 737 varies depending on the specific model, weight, and environmental conditions. Generally, the engines produce thrust ranging from about 20,000 to 30,000 pounds per engine, with a total required thrust for takeoff typically around 80,000 to 100,000 pounds. This thrust allows the aircraft to achieve the necessary speed for liftoff, usually around 150 to 180 knots, depending on the configuration and load.
Enough to lift a small rocket 5-600 feet.
The amount of thrust depends on the power of the engine
The 747-200 has engines rated at 55,145 pounds of thrust. This equated to 87,325 hp.
A jet engine can produce heat in the range of 1,600 to 2,000 degrees Celsius (2,900 to 3,600 degrees Fahrenheit) during operation. This intense heat is necessary for the engine to efficiently combust fuel and create the thrust needed for flight.
20 mil us dollar
The SR-71's J58 engine produces 142 kilo-newtons (32,000 pounds) of thrust.