Weight of Aircraft for given Excess Power Calculator

✖Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft.ⓘ Excess Power [P_excess]			+10% -10%
✖The Rate of Climb (RoC) is defined as the aircraft's vertical speed – the positive or negative rate of altitude change with respect to time.ⓘ Rate of Climb [RC]			+10% -10%

✖Aircraft Weight is the total aircraft weight at any moment during the flight or ground operation.ⓘ Weight of Aircraft for given Excess Power [W]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Climbing Flight Formulas PDF PDF Image

Weight of Aircraft for given Excess Power Solution

STEP 0: Pre-Calculation Summary

Formula Used

Aircraft Weight = Excess Power/Rate of Climb
W = P_excess/RC
This formula uses 3 Variables

Variables Used

Aircraft Weight - (Measured in Newton) - Aircraft Weight is the total aircraft weight at any moment during the flight or ground operation.
Excess Power - (Measured in Watt) - Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft.
Rate of Climb - (Measured in Meter per Second) - The Rate of Climb (RoC) is defined as the aircraft's vertical speed – the positive or negative rate of altitude change with respect to time.

STEP 1: Convert Input(s) to Base Unit

Excess Power: 37197.6 Watt --> 37197.6 Watt No Conversion Required
Rate of Climb: 3.71976 Meter per Second --> 3.71976 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

W = P_excess/RC --> 37197.6/3.71976

Evaluating ... ...

W = 10000

STEP 3: Convert Result to Output's Unit

10000 Newton --> No Conversion Required

FINAL ANSWER

10000 Newton <-- Aircraft Weight

(Calculation completed in 00.004 seconds)

You are here -

Home » Physics » Aircraft Mechanics » Aircraft Performance » Aerospace » Climbing Flight » Weight of Aircraft for given Excess Power

Credits

Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has verified this Calculator and 200+ more calculators!

< Climbing Flight Calculators

Flight path angle at given rate of climb

LaTeX Go Flight Path Angle = asin(Rate of Climb/Velocity)

Velocity of aircraft at given rate of climb

LaTeX Go Velocity = Rate of Climb/sin(Flight Path Angle)

Rate of Climb

LaTeX Go Rate of Climb = Velocity*sin(Flight Path Angle)

Weight of Aircraft for given Excess Power

LaTeX Go Aircraft Weight = Excess Power/Rate of Climb

Weight of Aircraft for given Excess Power Formula

LaTeX Go

Aircraft Weight = Excess Power/Rate of Climb
W = P_excess/RC

What angle do planes take off?

Planes slowly angle up during take off at about 2-3 degrees per second for a Boeing 747. The average passenger plane has a maximum take-off angle of about 10-15 degrees.

How to Calculate Weight of Aircraft for given Excess Power?

Weight of Aircraft for given Excess Power calculator uses Aircraft Weight = Excess Power/Rate of Climb to calculate 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 calculate Weight of Aircraft for given Excess Power using this online calculator? To use this online calculator for Weight of Aircraft for given Excess Power, enter Excess Power (P_excess) & Rate of Climb (RC) and hit the calculate button. Here is how the Weight of Aircraft for given Excess Power calculation can be explained with given input values -> 10007.43 = 37197.6/3.71976.

FAQ

What is Weight of Aircraft for given Excess Power?

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 and is represented as W = P_excess/RC or Aircraft Weight = Excess Power/Rate of Climb. Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft & The Rate of Climb (RoC) is defined as the aircraft's vertical speed – the positive or negative rate of altitude change with respect to time.

How to calculate Weight of Aircraft for given Excess Power?

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 is calculated using Aircraft Weight = Excess Power/Rate of Climb. To calculate Weight of Aircraft for given Excess Power, you need Excess Power (P_excess) & Rate of Climb (RC). With our tool, you need to enter the respective value for Excess Power & Rate of Climb and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

Home

FREE PDFs

🔍 Search