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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. Check FAQs
RC=vsin(γ)
RC - Rate of Climb?v - Velocity?γ - Flight Path Angle?

Rate of Climb Example

With values
With units
Only example

Here is how the Rate of Climb equation looks like with Values.

Here is how the Rate of Climb equation looks like with Units.

Here is how the Rate of Climb equation looks like.

3.7176Edit=60Editsin(0.062Edit)
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Rate of Climb Solution

Follow our step by step solution on how to calculate Rate of Climb?

FIRST Step Consider the formula
RC=vsin(γ)
Next Step Substitute values of Variables
RC=60m/ssin(0.062rad)
Next Step Prepare to Evaluate
RC=60sin(0.062)
Next Step Evaluate
RC=3.71761717802449m/s
LAST Step Rounding Answer
RC=3.7176m/s

Rate of Climb Formula Elements

Variables
Functions
Rate of Climb
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.
Symbol: RC
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Velocity
Velocity is a vector quantity (it has both magnitude and direction) and is the rate of change of the position of an object with respect to time.
Symbol: v
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.
Flight Path Angle
Flight Path Angle is defined as the angle between horizontal and the flight velocity vector, which describes whether the aircraft is climbing or descending.
Symbol: γ
Measurement: AngleUnit: rad
Note: Value should be greater than 0.
sin
Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse.
Syntax: sin(Angle)

Other Formulas to find Rate of Climb

​Go Rate of Climb for given excess power
RC=PexcessW
​Go Rate of Climb of Aircraft
RC=Pa-PrW

Other formulas in Climbing Flight category

​Go Flight path angle at given rate of climb
γ=asin(RCv)
​Go Velocity of aircraft at given rate of climb
v=RCsin(γ)
​Go Weight of Aircraft for given Excess Power
W=PexcessRC
​Go Excess power for given rate of climb
Pexcess=RCW

How to Evaluate Rate of Climb?

Rate of Climb evaluator uses Rate of Climb = Velocity*sin(Flight Path Angle) to evaluate the Rate of Climb, The Rate of Climb is the vertical speed at which an aircraft ascends. This formula calculates the rate of climb based on the aircraft's velocity and the sine of the flight path angle during the climb. Understanding and applying this formula is essential for pilots and engineers to optimize ascent performance, ensuring efficient and safe climb operations. Rate of Climb is denoted by RC symbol.

How to evaluate Rate of Climb using this online evaluator? To use this online evaluator for Rate of Climb, enter Velocity (v) & Flight Path Angle (γ) and hit the calculate button.

FAQs on Rate of Climb

What is the formula to find Rate of Climb?
The formula of Rate of Climb is expressed as Rate of Climb = Velocity*sin(Flight Path Angle). Here is an example- 3.717617 = 60*sin(0.062).
How to calculate Rate of Climb?
With Velocity (v) & Flight Path Angle (γ) we can find Rate of Climb using the formula - Rate of Climb = Velocity*sin(Flight Path Angle). This formula also uses Sine (sin) function(s).
What are the other ways to Calculate Rate of Climb?
Here are the different ways to Calculate Rate of Climb-
  • Rate of Climb=Excess Power/Aircraft WeightOpenImg
  • Rate of Climb=(Power Available-Power Required)/Aircraft WeightOpenImg
Can the Rate of Climb be negative?
No, the Rate of Climb, measured in Speed cannot be negative.
Which unit is used to measure Rate of Climb?
Rate of Climb is usually measured using the Meter per Second[m/s] for Speed. Meter per Minute[m/s], Meter per Hour[m/s], Kilometer per Hour[m/s] are the few other units in which Rate of Climb can be measured.
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