Phoenix Project

November 16th 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 C

Coolant outlet: 25 C

Coolant Flow: 100 l/min

 

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