Project Aegis Preliminary Design Review Team Members:

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Presentation transcript:

Project Aegis Preliminary Design Review Team Members: Yvonne Villapudua, Janet Blancas, Jimmy Lopez, Isabella Molina, and Lillian Chang

Launch Vehicle

Launch Dimensions Dimensions: Length: 119.00” Diameter: 6.08” Rebecca

Launch Vehicle Materials Main materials: Blue Tube 2.0 Aircraft Plywood

Stability, Center of Gravity, and Center of Pressure CG CP Stability Margin with Motor: 2.47 CG   CP Stability Margin without motor: 4.60

Motor Selection

General Motor Information The selected motor is an Aerotech L1170-FJ Diameter: 75mm Length: 26.18” Launch weight is 9.68lbs Empty weight is 3.51lbs

Motor Characteristics Burn time 3.71s Maximum thrust of 1489N Average thrust of 1136.9N Total impulse of 4222.6Ns

Motor Thrust Curve of Aerotech L1170-FJ

Thrust to Weight Ratio The thrust to weight ratio is 7.5 The launch vehicle must have a thrust greater than the weight of the launch vehicle in order to take off

Launch Vehicle Subsystems

Propulsion Subsystem Motor Motor retainer Motor mount

Structural and Aerodynamic Stability Subsystem Fins Nose Cone Airframe

Recovery Subsystem Components Parachutes Avionics Bay Electrical Components TeleGPS Main Parachute Compartment Drogue Parachute Compartment Avionics Bay Payload Bay

Avionics Bay Bulk Plates U-bolt Ejection Canisters Hole for wires Terminal Block

Electrical Components Missile Work RRC2+ Altimeter E-matches Batteries Key Switches Bulk Plate and Attached Components

Electronic Schematics

TeleGPS TeleGPS/Ground Station TeleDongle 3-Element Yagi Antenna 434.55 MHz 10 mW

Fragile Material Protection Payload

Primary Payload Design

Individual Components Container lid Inner Chamber Rack Inner Chamber Outer Shell Radiation shield

Inner Rack

Requirement Compliance Plan

Requirement Compliance Plan Launch Vehicle Requirement Compliance Plan Reusable rocket Recording official altitude Launch success Vehicle Prohibition Logan

Recovery System Requirement Compliance Plan Ground ejection test Deployment Electronics

Fragile Material Protection Requirement Compliance Plan Multiple Objects Unknown object

Safety Requirement Compliance Plan Launch and Safety checklist Safety Officer Rules and Regulation