Flight simulation

No simulation run yet — click "Run simulation" to integrate the ascent and descent.

Stability

CGCPStatic margin: 1.63 cal (stable)

Forces in ascent

Weight (mg)ThrustDragNormal force (CP)CG
Dry mass
49.8 g
Wet mass
61.5 g
CG (wet)
30.9 cm
CP
34.9 cm
CN_alpha total
26.58
— nose
2.00
— fins
24.58
Static margin
1.63 cal