Simulator of trajectory for comparison rockets to LEO orbits

Comparison of rockets from ground, aircraft, and baloon (with initial variables) Gravitation, Drag, friction, LEO, payload

Comparison of rockets from ground, aircraft, and baloon (with initial variables). Calculating with variable gravitation, drag, friction, and more. The result is the highest possible payload for initial variables, the second result is physical variables which govern these results. Two trajectories are possible to choose - constant angle and parabolic. Rocket is based on Virgin orbit rocket, it has two stages.