This project uses the equations of motion (DVAT equations) to model the flight of a model rocket. This includes drag and parachute deployment but does include the rocket losing weight. The rocket drifts to the right, representing wind, and plots the altitude over time. Max Altitude is reported. Challenge: Change the thrust, burn time, mass, and/or parachute drag so the path just touches the top of the tree line and the rocket lands on the landing pad.
