Phoenix Project November 16^th 2000
Test Conditions Oxidizer: GOX Fuel: Solid HTPB Feed Line Pressure: 20 Bar Start Up: Pirotecnic Ignitor Nozzle: Chopper (Water Cooled) Firing time: 8 sec	· Start Up - 00:00	· 01:00
· 03:00	· 05:00	· 07:00
· Oxidizer Shut Off – 07:50	· Shut Down – 8:00	Test Results Chamber Pressure: 10 Bar Mean Regression Rate: 2 mm/sec Thrust: 300 N Coolant inlet: 18 ºC Coolant outlet: 25 ºC Coolant Flow: 100 l/min