HM-7 Test Fire Successful

Cal Poly Space Systems conducted a successful short duration test fire of Hybrid Motor 7.

The design parameters of this engine are:
Thrust: 400 lbs
Burn time: 12 s
Fuel: Hydroxyl Terminated Polybutadiene (HTPB)
Oxidizer: Nitrous Oxide (N2O)

still frame

Check out just the burn here.
Check out the full test video here.