apogee and lifting off speed as a function of mass) Parachutes with external trigger functions
Barrowman equations for lift coefficients (optional).International Standard Atmosphere (1976).Solved using LSODA with adjustable error tolerances.Rigorous treatment of mass variation effects.Main features Nonlinear 6 degrees of freedom simulations Furthermore, the implementation facilitates complex simulations, such as multi-stage rockets, design and trajectory optimization and dispersion analysis. Weather conditions, such as wind profile, can be imported from sophisticated datasets, allowing for realistic scenarios. The code is written as a Python library and allows for a complete 6 degrees of freedom simulation of a rocket's flight trajectory, including high fidelity variable mass effects as well as descent under parachutes. RocketPy is the next-generation trajectory simulation solution for High-Power Rocketry.
