Rate of Climb 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%
✖Aircraft Weight is the total aircraft weight at any moment during the flight or ground operation.ⓘ Aircraft Weight [W]			+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 for given excess power [RC]

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Rate of Climb for given excess power Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

Variables Used

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.
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.
Aircraft Weight - (Measured in Newton) - Aircraft Weight is the total aircraft weight at any moment during the flight or ground operation.

STEP 1: Convert Input(s) to Base Unit

Excess Power: 37197.6 Watt --> 37197.6 Watt No Conversion Required
Aircraft Weight: 10000 Newton --> 10000 Newton No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

RC = P_excess/W --> 37197.6/10000

Evaluating ... ...

RC = 3.71976

STEP 3: Convert Result to Output's Unit

3.71976 Meter per Second --> No Conversion Required

FINAL ANSWER

3.71976 Meter per Second <-- Rate of Climb

(Calculation completed in 00.004 seconds)

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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

Rate of Climb for given excess power Formula

LaTeX Go

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

What is the best angle of climb speed?

The best angle of climb speed of an aircraft gets you the greatest altitude per unit of ground distance (feet per mile).

How to Calculate Rate of Climb for given excess power?

Rate of Climb for given excess power calculator uses Rate of Climb = Excess Power/Aircraft Weight to calculate the Rate of Climb, The Rate of Climb for given Excess Power is the vertical speed at which an aircraft ascends, determined by the excess power available. Excess power represents the surplus power available beyond what is required to maintain level flight. Rate of Climb is denoted by RC symbol.

How to calculate Rate of Climb for given excess power using this online calculator? To use this online calculator for Rate of Climb for given excess power, enter Excess Power (P_excess) & Aircraft Weight (W) and hit the calculate button. Here is how the Rate of Climb for given excess power calculation can be explained with given input values -> 3.71976 = 37197.6/10000.

FAQ

What is Rate of Climb for given excess power?

The Rate of Climb for given Excess Power is the vertical speed at which an aircraft ascends, determined by the excess power available. Excess power represents the surplus power available beyond what is required to maintain level flight and is represented as RC = P_excess/W or Rate of Climb = Excess Power/Aircraft Weight. Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft & Aircraft Weight is the total aircraft weight at any moment during the flight or ground operation.

How to calculate Rate of Climb for given excess power?

The Rate of Climb for given Excess Power is the vertical speed at which an aircraft ascends, determined by the excess power available. Excess power represents the surplus power available beyond what is required to maintain level flight is calculated using Rate of Climb = Excess Power/Aircraft Weight. To calculate Rate of Climb for given excess power, you need Excess Power (P_excess) & Aircraft Weight (W). With our tool, you need to enter the respective value for Excess Power & Aircraft Weight and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Rate of Climb?

In this formula, Rate of Climb uses Excess Power & Aircraft Weight. We can use 2 other way(s) to calculate the same, which is/are as follows -

Rate of Climb = Velocity*sin(Flight Path Angle)
Rate of Climb = (Power Available-Power Required)/Aircraft Weight

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