Complex motion equation (projectile with changing mass and thrust)

In summary, calculating the trajectory of a projectile with changing mass involves using Newton's second law of motion and integrating the equations of motion. Factors such as initial velocity, ejected propellant mass and velocity, launch angle, and gravity all affect the motion of the projectile. Thrust, which is affected by the ejected propellant, can significantly alter the projectile's acceleration and velocity. Differential equations are used to model the complex motion of the projectile, but accuracy can be affected by external factors and small errors in measurement or calculation.
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kaycha
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I need an equation to predict the flight path of a changing mass projectile under changing thrust. Any thoughts?
 
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kaycha said:
I need an equation to predict the flight path of a changing mass projectile under changing thrust. Any thoughts?
General as stated, you have to do numerical integration of Newtons laws of motion. For specific thrust & mass profiles there might an analytical solution.
 
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