Application to calculate the parachute diameter required for a given mass and descent velocity, considering varying air densities at different altitudes.
- Python
- Numpy
- Matplotlib
- Tkinter (for interface)
-
Run the script:
python interface.py
-
Input Parameters:
- Minimum Mass (kg): Lower bound of the rocket mass range.
- Maximum Mass (kg): Upper bound of the rocket mass range.
- Descent Velocity (m/s): Target descent velocity.
- Drag Coefficient: Coefficient of drag for the parachute.
- Altitude (km): Altitude at which target descent velocity should be reached (air density is calculated here).
-
Update Plot:
- Click the Update Plot button to calculate and display the results.
-
Plot Description:
- Blue Curve: Required parachute diameter for the specified mass range.
- Dashed Black Lines: Standard Rocketman parachute sizes with labels in inches.
