1. UPDATE #2

3.  The predicted altitude was ~9500 feet.  Actual altitude was ~11960 feet.  After investigation the error was found in the simulated weight of the rocket.  Simulated Dry Weight 17.5 lbs  Actual Dry Weight 14.35 lbs

4.  Propellant type has low values for burn rate coefficient and exponent.  Simulated to fly 8250 feet.  Liftoff Weight  Motor Housing 3.8 lbs  Propellant 3.554 lbs  Rocket Dry 14.35 lbs  Liftoff weight 21.704 lbs

6.  On Nov 7 th a member of next semester’s project will be achieving his level I and II certification flights.  This puts the next project team 1 semester ahead of where we started.

7.  Launch Date for ODU Rocket Team’s final launch.  If successful flight occurs as simulated on this launch the project goals are 100% complete.