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→Vehicle Criteria
# At apogee, drogue chute deploys
# At apogee, drogue chute deploys
# Rocket descends and main chute deploys
# Rocket descends and main chute deploys
[[File:Events_Diagram-2.jpg|thumb|alt=A summary of the rocket's intended flight actions|Charybdis Rocket Events|upright=0.9|right|Flight Events Sequence]]
[[File:Events_Diagram-2.jpg|thumb|alt=A summary of the rocket's intended flight actions|Charybdis Rocket Events|upright=0.9|right|Flight Events Sequence]]
The mission will be considered successful if the rocket unit reaches spin stabilization, demonstrates successful de-spin prior to reaching apogee. The rocket must be recovered intact and reusable and pass the L3 certification inspection authorized by Tripoli.
The mission will be considered successful if the rocket unit reaches spin stabilization, demonstrates successful de-spin prior to reaching apogee. The rocket must be recovered intact and reusable and pass the L3 certification inspection authorized by Tripoli.
== Constraints ==
== Constraints ==