Thrust given Mass and Acceleration of Rocket Calculator

✖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 [a]			+10% -10%

✖Thrust is the force produced by the expulsion of high-speed exhaust gases from a rocket engine.ⓘ Thrust given Mass and Acceleration of Rocket [F]

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Thrust given Mass and Acceleration of Rocket Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

Variables Used

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.
Acceleration - (Measured in Meter per Square Second) - Acceleration is the rate of change of velocity with respect to time.

STEP 1: Convert Input(s) to Base Unit

Mass of Rocket: 420.5 Kilogram --> 420.5 Kilogram No Conversion Required
Acceleration: 13.85 Meter per Square Second --> 13.85 Meter per Square Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

F = m*a --> 420.5*13.85

Evaluating ... ...

F = 5823.925

STEP 3: Convert Result to Output's Unit

5823.925 Newton --> No Conversion Required

FINAL ANSWER

5823.925 Newton <-- Thrust

(Calculation completed in 00.021 seconds)

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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

Thrust given Mass and Acceleration of Rocket Formula

LaTeX Go

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

What is thrust?

Thrust is a reaction force, When a system expels or accelerates mass in one direction, the accelerated mass will cause a force of equal magnitude but in opposite direction, to be applied to that system. The force applied on a surface in a direction perpendicular to the surface is also called thrust.

How to Calculate Thrust given Mass and Acceleration of Rocket?

Thrust given Mass and Acceleration of Rocket calculator uses Thrust = Mass of Rocket*Acceleration to calculate the Thrust, Thrust given Mass and Acceleration of Rocket formula is defined as the relationship between the mass of the rocket and its acceleration, illustrating how the force generated propels the rocket forward in space. Thrust is denoted by F symbol.

How to calculate Thrust given Mass and Acceleration of Rocket using this online calculator? To use this online calculator for Thrust given Mass and Acceleration of Rocket, enter Mass of Rocket (m) & Acceleration (a) and hit the calculate button. Here is how the Thrust given Mass and Acceleration of Rocket calculation can be explained with given input values -> 1.9944 = 420.5*13.85.

FAQ

What is Thrust given Mass and Acceleration of Rocket?

Thrust given Mass and Acceleration of Rocket formula is defined as the relationship between the mass of the rocket and its acceleration, illustrating how the force generated propels the rocket forward in space and is represented as F = m*a or Thrust = Mass of Rocket*Acceleration. The Mass of Rocket is its stated mass at any given point in time while the rocket is in motion & Acceleration is the rate of change of velocity with respect to time.

How to calculate Thrust given Mass and Acceleration of Rocket?

Thrust given Mass and Acceleration of Rocket formula is defined as the relationship between the mass of the rocket and its acceleration, illustrating how the force generated propels the rocket forward in space is calculated using Thrust = Mass of Rocket*Acceleration. To calculate Thrust given Mass and Acceleration of Rocket, you need Mass of Rocket (m) & Acceleration (a). With our tool, you need to enter the respective value for Mass of Rocket & Acceleration 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 Thrust?

In this formula, Thrust uses Mass of Rocket & Acceleration. We can use 2 other way(s) to calculate the same, which is/are as follows -

Thrust = Mass Flow Rate*Exit Velocity
Thrust = 1000*Power in Jet/[c]

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