Astrodynamic articles
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Rocket Aerodynamics Calculator
Rocket Parameters
Results
Drag Coefficient
0.00
Center of Pressure
0.00 m
Center of Mass
0.00 m
Drag Force
0.00 N
Aerodynamic Stability
0.00 (calibers)
Mach Number
0.00
Atmospheric Density
0.00 kg/m³