Classic Concept
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)
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
HTPB Fuel Grain (Solid Fuel) Pre-Combustion Chamber Moldable Ceramic, acts also as an insulator for the composite shell M-NPT Threading Nitrous Oxide Tank (Liquid Fuel)
Post-Combustion Chamber Moldable Ceramic, acts also as an insulator for the composite shell HTPB Fuel Grain (Solid Fuel) Graphite Nozzle – Currently has the exact specifications as the steel rocket