1. R0X-56 Design

2. 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 Reinforced)

3. Micro IMU Provides serial digital outputs of tri- axial acceleration, rate of turn (gyro) and tri-axial magnetic field data. Payload Pico-Satellite Electronics Avionics and Data Acquisition Helium Reservoir Vessel – Provides better thrust vectoring because of its smaller molecular weight (compared to NOS). Helium is also less sensitive to extreme temperatures

4. HTPB Fuel Grain (Solid Fuel) Hybrid Fuel Mixing Zone Pre-Combustion Chamber Moldable Ceramic, acts also as an insulator for the composite shell Note: Components will be wrapped with composite skin to hold them in place. M-NPT Threading Nitrous Oxide Tank (Liquid Fuel)

5. Pre-Combustion Chamber Moldable Ceramic, acts also as an insulator for the composite shell HTPB Fuel Grain (Solid Fuel) Note: Components will be wrapped with composite skin to hold them in place. Hybrid Fuel Mixing Zone Graphite Nozzle – Currently has the exact specifications as the steel rocket