Weight of Aircraft for given Excess Power evaluator uses Aircraft Weight = Excess Power/Rate of Climb to evaluate the Aircraft Weight, The Weight of Aircraft for given Excess Power refers to the force exerted by gravity on the mass of the aircraft, it's the sum of the mass of all components of the aircraft, including the airframe, payload (passengers, cargo), fuel, and any other items onboard, this equation suggests that the weight of the aircraft can be calculated based on the excess power available during climb flight and the rate of climb. Aircraft Weight is denoted by W symbol.
How to evaluate Weight of Aircraft for given Excess Power using this online evaluator? To use this online evaluator for Weight of Aircraft for given Excess Power, enter Excess Power (Pexcess) & Rate of Climb (RC) and hit the calculate button.