NG12 said:Homework Equations
The Attempt at a Solution
I am not sure of an equation to use for this problem
The thrust of a model rocket is calculated by multiplying the mass of the rocket's propellant by the velocity of the exhaust gases as they leave the rocket's engine.
The formula for calculating thrust is: T = m * v, where T is the thrust in Newtons, m is the mass of the propellant in kilograms, and v is the velocity of the exhaust gases in meters per second.
The mass of the propellant can be determined by weighing the rocket before and after the launch. The difference between the two weights is the mass of the propellant.
The average velocity of exhaust gases for a model rocket is typically between 400-1000 meters per second. However, this can vary depending on the specific engine used.
The acceleration of a model rocket can be calculated by dividing the thrust value by the total mass of the rocket (including the propellant). This will give you the acceleration in meters per second squared (m/s^2).