Please redefine your question, what exactly do you want t know? Jet engines can produce power in a multitude of ways, either thrust delivered through exhaust gasses in Newtons per square Meter, of they can deliver power through the shaft in the jet engine which would deliver a torque power. (Most modern jet engines utilized in aircraft by the way produce both, thrust for the propulsion of the aircraft and torque to power all accessory devices such as fuel pumps, oil pumps and hydraulic pumps.
If you're referring to the power of the engine, it is not in hertz. The power of of a jet engine is measured in pounds.
The speed of the jet engine depends on the power, model and the year in which it is made.Old jet engines are weak and do not generate much power.
Depends on which model and brand of jet engine you are asking about. There have been many jet engines designed and built by many different companies over the years.
I cannot give you a specific answer, because it varies depending on the engine.
Thrust is the power made by a jet engine to propel an aircraft.
Both Frank Whittle and Hans von Ohain started creating a jet engine at the same time. Whittle created the first working jet engine, but Ohain was the first to power an aircraft
A helicopter with a jet engine. The engine is adapted to give power to a transmission, rather than thrust.
An aeroderivative gas turbine is a type of gas turbine engine that is derived from jet engines used in aircraft. These engines are designed to be more lightweight, compact, and efficient than industrial gas turbines, making them a popular choice for power generation in applications where quick start-up and flexibility are important. They are typically used in combined cycle power plants, as backup power for industries, and in mobile power generation units.
jet engine
You must mean 'Thrust' . The thrust is the amount of power the jet engine supplies.
It was invented during WW2 by 'Power Jets' ,a company led by Sir Frank Whittle to increase power and efficiency of early jet engines.
A typicial Auxiliary Power Unit (APU) is a turboshaftengine. It is similar to a jet engine with how it's compressor and turbine sections are laid out. However jet engines provide power through thrust (exhaust gas pressure) whereas turboshaft engines provide power through a shaft attached to either the compressor or turbine section.