1. P07109: Project M.E.T.E.O.R. Flying Rocket Team Andrew ScarlataProject Leader/ Mechanical Engineer Geoff CassellLead Engineer/ Mechanical Engineer David HallLead Engineer/ Mechanical Engineer Luke CadinMechanical Engineer Zack MottMechanical Engineer Garett PickettElectrical Engineer Brian WhitbeckMechanical Engineer Sponsor: Dr. Dorin Patru Electrical Engineering department Advisor: Dr. Jeffrey Kozak Generous donation from Harris RF Corporation

2. Project Description  Part of the M.E.T.E.O.R. family –Launching small payloads into low-Earth orbit –Continuation of P06006: Hybrid Rocket Engine Design and Testing –Working in conjunction with P07105 & P07106  Research, develop, and manufacture a flight ready hybrid rocket stage  Achieve a structure to propellant ratio of 1:10 –The highest acceptable value is 2:10  As of now, there are two potential concepts –Chalice –Embedded Fuel Grain

3. Chalice Design HTPB Fuel Grain Nitrous Oxide Tank Pre-Combustion Chamber Post-Combustion Chamber Graphite Nozzle Helium Reservoir Electronics Payload Micro IMU (Inertial Measurement Unit) Composite Outer Shell (Aluminum Inner Reinforced)

4. Embedded Fuel Grain HTPB Fuel Grain Nitrous Oxide Tank Pre-Combustion Chamber Post-Combustion Chamber Graphite Nozzle Helium Reservoir Vessel Electronics Payload Micro IMU (Inertial Measurement Unit) Composite Outer Shell (Aluminum Inner Liner) Siphon Tube