Project Lead: Austin Brenner

Slides:

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Presentation transcript:

Project Lead: Austin Brenner UIowa AIAA MAV Team Project Lead: Austin Brenner

Team Roster Advisor: Kevin Trojanowski Members: Vicki, Ryan, Alec, Andrew, Matt, and Frank

Rocket Design Material: Fiberglass Static stability Margin:2.17cal* Weight, cost, manufacturability Static stability Margin:2.17cal*

Structure Systems Nosecone: Ogive 4 Polypropylene Fins: 4x Carbon Fiber 1/16” plate h=5” root=6” tip=6” angle=30°

AGSE Design will capture, contain, and launch the payload Material: aluminium, steel, rubber, acrylic. Servo conveyor systems Linear Actuators Servo Winch Proximity switches Torsion Springs

Recovery System Parachute selection Dual deployment system Testing

Drag System Geometry selection Control Programming

Control System Sensor selection Accelerometer, Altitude/Pressure, Temperature, IR Receiver Safety kill switch for failure to launch Controller software design System interaction

Control System Options

Cargo Bay System Rotating inner cylinder Secure Payload Controls Servo motor Light dependent resistor

Motor Selection K261-P Motor Weight increase Drag system to bring down altitude Simulated using OpenRocket software

Exit Rail Velocity - 13.4 m/s Apogee - 1144 m ~ 3753 ft Exit Rail Velocity - 16.7 m/s Apogee - 1632 m ~ 5354 ft

Propulsion Parameters Thrust to Weight: ~9.108 Rail Exit Velocity: 16.7 m/s Max Velocity: 249 m/s Max Acceleration: 66.1 m/s2

Safety/ Risk

Verification and Testing Drag/Payload bay motor test Drag system CFD analysis Ground recovery system test of linear actuators and servo conveyors for AGSE.

Questions?

Sources https://www.apogeerockets.com/Intro_to_Dual_Deployment_in_Rocketry