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Published byHunter Henshaw
Modified over 4 years ago
Battery PDB Controller GPS Data Recorder Antenna Cam Lower Stage Harness Upper portLower port Upper port Lower Stage Harness Sensors Cam Avionics Layout
Combustion Chamber Shock CordParachute Ejection Plate Chute retention film Bulkhead Composite layer sep point Squib Cardboard (internal tube) layer sep point Parachute Subassembly Layout Bulkhead
High School Payload Competition Avionics Payload Bay Layout
2 nd Stage Engine Mount
1 st Stage Electronics and Recovery Bay Battery Controller 1 st Stage Main Chute Combustion Chamber
1 st Stage Engine Mount
Second Stage, Avionics, Payload First Stage
Payload Bay Drogue Chute Assembly Main Chute Assembly Avionics Bay 2 nd Stage Engine Mount 1 st Stage Engine Mount 1 st Stage Electronics/ Recovery
University of Florida PDR Presentation. Vehicle Design Diameter: 5.86 Length: 135 Static Stability Margin: 1.4 Total Weight: 23.6 lbs.
BYU Rocket Team Special thanks to:
Madison West SLI '06 New Team. Vehicle Mission Statement ● Successfully launch rocket to 5,280 feet. ● Capture multiple simultaneous images in the standard.
Preliminary Design Review. Rocket & Payload Schematic.
Preliminary Design Review University of Colorado Boulder NASA Student Launch
D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB PDR PRESENTATION 1.
P RELIMINARY D ESIGN R EVIEW University of North Dakota Frozen Fury Rockety Team.
Critical Design Review ….. Royal Ordnance,Summerfield 17 th February 2001 National Rocketry Competition 2001 Open Rocketry Association Slide 1/14.
“ The Other Woman ” National Association of Rocktry Level Three Certification Project By Steve Laird NAR #86948.
Critical Design Review NASA University Student Launch Initiative University of Nebraska–Lincoln
Launch Lug – helps to guide the rocket upward until it reaches enough velocity for the fins to engage. Parachute – assists in the safe recovery of the.
Rocket Based Deployable Data Network University of New Hampshire Rocket Cats Collin Huston, Brian Gray, Joe Paulo, Shane Hedlund, Sheldon McKinley, Fred.
U NIVERSITY OF F LORIDA I NTIMI GATOR PDR. O UTLINE Project Organization Vehicle Design Payload Design Recovery System Component Testing Subscale Flight.
Our Mission Statement Launch a high-power rocket to an altitude of one mile carrying the Operation: Epic Beep payload package. At lift off, the rocket’s.
NASA SLI 2010 Mulberry Grove High School Critical Design Review Measurement of UVB Radiation Absorption by Cloth Material at Different Altitudes and Measurement.
Critical Design Review “The Distribution of Ionizing Radiation with Altitude” Left to Right: Izzy S.- Audio Visual Tom L.- Payload James Z.-Construction.
RezRiders. Mission statement Through the USLI program the Northwest Indian College Space Center’s RezRiders Team enhances its involvement in science,
Flight Readiness Review March Vehicle Criteria Testing and vehicle design Bulkheads: 9-Ply ½” birch plywood made by Public Missiles, Ltd or ¼ inch.
NASA CDR Presentation Spring Grove Area High School.
St. Vincent – St. Mary FRR Presentation NASA Student Launch Initiative.
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