byu rocket team 2009-2010
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BYU Rocket Team 2009-2010. Special thanks to: Boise Discovery Teens Club Jeff Smith Dr. David Fullwood. Outline. About the Competition About the Rocket Nose Body Fins Flight Plan Electronics Deployments Simulations Motor Recovery Plan. The Competition. - PowerPoint PPT PresentationTRANSCRIPT
BYU Rocket Team 2009-2010
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Special thanks to:Boise Discovery Teens ClubJeff SmithDr. David Fullwood
Outline About the Competition About the Rocket
Nose Body Fins Flight Plan
Electronics Deployments Simulations
Motor Recovery Plan
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The Competition Intercollegiate Rocket Engineering
Competition (June 17, 2010) Sponsored by ESRA Goals:
Design, build, and launch a rocket to reach 10,000 feet AGL
Minimum 10-lb payload Closest to 10,000 feet wins Rocket must reach at least 5000
feet and not exceed 12,000 feet to receive points for altitude
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Last Year One successful Launch Learned lots of basics Most components were pre-fabricated
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This Year Still learning the basics Manufacturing most components “in house” Building off of last year’s design
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Design OverviewNose Cone
Body – 1: Payload
Body – 2: Chute Storage
Body – 3: Motor and Fins Coupler 3:
Tail Drogue
Coupler 2:Altimeter
Coupler 1:Nose Drogue
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Nose
Design Ogive shape will provide the best
aerodynamics for our anticipated velocity (760 ft/s)
Contour based on last year’s design Manufacturing
Created a wood form on a lathe Currently preparing form for pre-
preg layup Integration
Coupler 1 will be rigidly fixed to the cone
Nose cone chute will attach to the nose cone bulkhead
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Body: Part 1 – Payload Bay
Body section will fit on to coupler 1 and be rigidly fixed to coupler 2
Payload Requirements Must weigh 10 pounds (competition rule) Must be fit inside body tube (design
team) Payload Design
Modified RC aircraft (Firebird) Deploy payload with main chute
(~1,500 feet) Remaining weight will be sand
Testing
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Body: Part 2 – Chute Storage
Integration Body section will fit on to
coupler 2 and be rigidly fixed to coupler 3
Main chute will attach to bulkhead 3
Main chutes will be stored here
Manufacturing Rolled carbon fiber 5 harness
pre-preg Cut to 46 inches
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Body: Part 3 – Motor and Fins
Motor will be housed here Manufacturing
Rolled carbon fiber 5 harness pre-preg
Cut to 46 inches Integration
Tail Drogue will attach to bulk head 4 Motor will mount inside body part 3 Body part 3 will slip fit over coupler 3 Slots will be cut for fins
Fins will attach to the bottom
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Fins
Trapezoidal Design Manufacturing
Aluminum plate (1/8”) Will be water jet cut to desired
dimensions Integration
Tabs will fit into body tube slots
Fins will be anchored with epoxy and mechanical fasteners
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Flight Plan - Overview Launch Deploy drogue chute before 10,000 feet (“zipperless” rear separation) Apogee should be very close to 10,000 feet – then fall about 8,500
feet Deploy main chute, nose cone and payload at 1,500 feet Recover all parts within 2 hours
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Flight Plan - Electronics AIM USB Altimeter ($115) 2 Deployments:
Main parachute Drogue (apogee or user defined)
Two 9V batteries for redundancy Our uses
Deploy brake system and drogues (drogue setting) Deploy main parachute (main setting)
Purchased 2 for deployment redundancy
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Flight Plan – Electronics (cont) Electronics Bay will be inside
coupler 3 Pressure sensor holes will
line up using a ‘belt’ of body tube material
Wires from altimeter attach to Davey Fire Electric Matches (low current).
Gunpowder inside Silly Pipe end cap ignites to pressurize body tube and eject recovery system.
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Flight Plan – Simulations
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Motor Minimum launch height
must be >10,000 feet M-motor will work ($750) Cessaroni L1115 will be
used for test launch (7,000 ft AGL) 4,908 N-sec Impulse (Full L)
Test Launch (May 22, 2010) With Utah Rocket Club Must be UNDER 10,000 ft FAA waiver NAR L2 Certification required
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Rent a 4x4 and small trailer Make sure we have at least 2 people at the
competition
Recovery Plan
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Schedule Right Now
Fabricate Components Purchase Parts/Expendables Assemble Rocket Test Sub-systems
Test launch – 5/22/2010 Competition launch – 6/17/2010
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Questions?
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