A python application that uses Euler's method to computationally solve the nonlinear, 2nd order differential equation that represents the vertical flight of a rocket. Uses 1st order approximations for atmospheric density and engine thrust data.

pip3 install -r requirements.txt

• pyqt5 - Qt with python bindings to build the GUI
• pyqtgraph - Graphing module for pyqt to render graphs
• numpy - Array data types for graphing (requirement of pyqtgraph)

??

http://www.dtic.mil/dtic/tr/fulltext/u2/729858.pdf - for coefficient of drag of a parachute