Acceleration of Rocket Calculator

✖Thrust is the force produced by the expulsion of high-speed exhaust gases from a rocket engine.ⓘ Thrust [F]			+10% -10%
✖The Mass of Rocket is its stated mass at any given point in time while the rocket is in motion.ⓘ Mass of Rocket [m]			+10% -10%

✖Acceleration is the rate of change of velocity with respect to time.ⓘ Acceleration of Rocket [a]

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Acceleration of Rocket Solution

STEP 0: Pre-Calculation Summary

Formula Used

Acceleration = Thrust/Mass of Rocket
a = F/m
This formula uses 3 Variables

Variables Used

Acceleration - (Measured in Meter per Square Second) - Acceleration is the rate of change of velocity with respect to time.
Thrust - (Measured in Newton) - Thrust is the force produced by the expulsion of high-speed exhaust gases from a rocket engine.
Mass of Rocket - (Measured in Kilogram) - The Mass of Rocket is its stated mass at any given point in time while the rocket is in motion.

STEP 1: Convert Input(s) to Base Unit

Thrust: 5825 Newton --> 5825 Newton No Conversion Required
Mass of Rocket: 420.5 Kilogram --> 420.5 Kilogram No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

a = F/m --> 5825/420.5

Evaluating ... ...

a = 13.8525564803805

STEP 3: Convert Result to Output's Unit

13.8525564803805 Meter per Square Second --> No Conversion Required

FINAL ANSWER

13.8525564803805 ≈ 13.85256 Meter per Square Second <-- Acceleration

(Calculation completed in 00.020 seconds)

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Credits

Created by Chilvera Bhanu Teja

Institute of Aeronautical Engineering (IARE), Hyderabad

Chilvera Bhanu Teja has created this Calculator and 300+ more calculators!

Verified by Vaibhav Malani

National Institute of Technology (NIT), Tiruchirapalli

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< Thrust and Power Generation Calculators

Power required to produce Exhaust Jet Velocity

LaTeX Go Power Required = 1/2*Mass Flow Rate*Exit Velocity^2

Thrust given Exhaust Velocity and Mass Flow Rate

LaTeX Go Thrust = Mass Flow Rate*Exit Velocity

Thrust given Mass and Acceleration of Rocket

LaTeX Go Thrust = Mass of Rocket*Acceleration

Acceleration of Rocket

LaTeX Go Acceleration = Thrust/Mass of Rocket

Acceleration of Rocket Formula

LaTeX Go

Acceleration = Thrust/Mass of Rocket
a = F/m

What is acceleration?

Acceleration is the rate of change of the velocity of an object with respect to time. Acceleration is a vector quantity, means it has both magnitude and direction.

How to Calculate Acceleration of Rocket?

Acceleration of Rocket calculator uses Acceleration = Thrust/Mass of Rocket to calculate the Acceleration, The Acceleration of rocket formula is defined as the ratio of thrust produced by rocket to mass of the rocket. Acceleration is denoted by a symbol.

How to calculate Acceleration of Rocket using this online calculator? To use this online calculator for Acceleration of Rocket, enter Thrust (F) & Mass of Rocket (m) and hit the calculate button. Here is how the Acceleration of Rocket calculation can be explained with given input values -> 40451.39 = 5825/420.5.

FAQ

What is Acceleration of Rocket?

The Acceleration of rocket formula is defined as the ratio of thrust produced by rocket to mass of the rocket and is represented as a = F/m or Acceleration = Thrust/Mass of Rocket. Thrust is the force produced by the expulsion of high-speed exhaust gases from a rocket engine & The Mass of Rocket is its stated mass at any given point in time while the rocket is in motion.

How to calculate Acceleration of Rocket?

The Acceleration of rocket formula is defined as the ratio of thrust produced by rocket to mass of the rocket is calculated using Acceleration = Thrust/Mass of Rocket. To calculate Acceleration of Rocket, you need Thrust (F) & Mass of Rocket (m). With our tool, you need to enter the respective value for Thrust & Mass of Rocket and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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