3DOF-Rocket-PU

Natalia Edith Mejia Bautista thesis work

3DOF Numerical simulator of rocket trajectory

Propulsion UNAM rocketry team

Implements different numerical integrators to solve ODEs *Euler *RK2 *RK4 *EulerAdaptive *RKF45

POO paradigm

1. Rocket, its motor and parachute
2. Flight environment
   • ISA atmosphere
   • Base wind and random gust
3. Launch site and rail