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Distance Required For Deceleration In Normal Braking Mode To Nominal Takeoff Speed Calculator

Formula Used:

\[ S3 = \frac{(Vt - 15)^2 - Vex^2}{8 \times d} \]

m/s
m/s
m/s²

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1. What is the Distance for Deceleration in Normal Breaking Mode?

The Distance for Deceleration in Normal Breaking Mode (S3) represents the distance required for an aircraft to decelerate from the threshold transition speed to the nominal turn-off speed during normal braking operations. This calculation is crucial for runway design and aircraft performance analysis.

2. How Does the Calculator Work?

The calculator uses the following formula:

\[ S3 = \frac{(Vt - 15)^2 - Vex^2}{8 \times d} \]

Where:

Explanation: The formula calculates the distance required for deceleration based on the difference between the adjusted threshold speed and nominal turn-off speed, divided by eight times the deceleration rate.

3. Importance of S3 Calculation

Details: Accurate S3 calculation is essential for runway safety design, determining appropriate runway lengths, and ensuring aircraft can safely decelerate to turn-off speeds under normal braking conditions.

4. Using the Calculator

Tips: Enter threshold speed in m/s, nominal turn-off speed in m/s, and deceleration rate in m/s². All values must be positive numbers greater than zero.

5. Frequently Asked Questions (FAQ)

Q1: Why is 15 subtracted from the threshold speed?
A: The 15 m/s adjustment accounts for the transition phase where the aircraft reduces speed from threshold speed to begin the normal braking deceleration phase.

Q2: What is a typical deceleration rate for aircraft?
A: Typical deceleration rates vary by aircraft type and braking system, but generally range from 2-4 m/s² for normal braking operations.

Q3: How does this differ from emergency braking distance?
A: Emergency braking would use higher deceleration rates and different calculations, as it assumes maximum braking effort rather than normal operational braking.

Q4: What factors affect the nominal turn-off speed?
A: Turn-off speed depends on aircraft category, weight, runway conditions, and taxiway design specifications.

Q5: Is this calculation used for all aircraft types?
A: While the formula is generally applicable, specific aircraft may have unique performance characteristics that require additional considerations in runway design.

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