In flight mechanics, “power required at the end of flight” refers to the amount of power that the aircraft’s engines or propulsion system must generate to sustain level flight at the end of the flight mission. It is an important parameter that pilots and engineers consider during flight planning and performance calculations.
Power required at the end of flight=(1000*v)/t
- v” typically represents the aircraft’s airspeed, which is the speed at which the aircraft is moving relative to the surrounding air.
- “t” represents the aircraft’s thrust, which is the force produced by the engines to propel the aircraft forward.
- 1000 is a constant factor, possibly used for unit conversion purposes.