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Project Aegis Preliminary Design Review Team Members:

Published byBeryl Greene Modified over 6 years ago

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Presentation on theme: "Project Aegis Preliminary Design Review Team Members:"— Presentation transcript:

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

2 Launch Vehicle

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

4 Launch Vehicle Materials
Main materials: Blue Tube 2.0 Aircraft Plywood

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

6 Motor Selection

7 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

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

9 Motor Thrust Curve of Aerotech L1170-FJ

10 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

11 Launch Vehicle Subsystems

12 Propulsion Subsystem Motor Motor retainer Motor mount

13 Structural and Aerodynamic Stability Subsystem
Fins Nose Cone Airframe

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

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

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

17 Electronic Schematics

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

19 Fragile Material Protection Payload

20 Primary Payload Design

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

22 Inner Rack

23 Requirement Compliance Plan

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

25 Recovery System Requirement Compliance Plan
Ground ejection test Deployment Electronics

26 Fragile Material Protection Requirement Compliance Plan
Multiple Objects Unknown object

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

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