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Published byHunter Henshaw
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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
BYU Rocket Team Special thanks to: Boise Discovery Teens Club Jeff Smith Dr. David Fullwood.
UCF_USLI Preliminary Design Review David Cousin Freya Ford Md Arif Drew Dieckmann Stephen Hirst Mitra Mossaddad University of Central Florida.
Critical Design Review NASA University Student Launch Initiative University of Nebraska–Lincoln
The Rocket Men Project One Giant Leap. Dimensions Rocket Length in. Rocket Mass- 171 oz. Top Body Tube Length in. Bottom Body Tube Length-
Critical Design Review Presentation Jan. 20, 2011.
Recovery Systems Tripoli Minnesota Gary Stroick December 2012.
Preliminary Design Review. Rocket & Payload Schematic.
Team Members:Tony Guzzo Eric Jacob Bill Liewehr Alex Schlaupitz Design of a Level 2 Rocket for the Wisconsin Space Grant Consortium Advisor: Dr. William.
Rocket Based Deployable Data Network University of New Hampshire Rocket Cats Collin Huston, Brian Gray, Joe Paulo, Shane Hedlund, Sheldon McKinley, Fred.
“ The Other Woman ” National Association of Rocktry Level Three Certification Project By Steve Laird NAR #86948.
Critical Design Review of “Mach Shock Reduction” Phase II January 2008 Statesville, NC.
U NIVERSITY OF F LORIDA I NTIMI GATOR PDR. O UTLINE Project Organization Vehicle Design Payload Design Recovery System Component Testing Subscale Flight.
Flight Readiness Review March Vehicle Criteria Testing and vehicle design Bulkheads: 9-Ply ½” birch plywood made by Public Missiles, Ltd or ¼ inch.
Safety ► The safety officer for the entire team is Maia Madrid. ► During launch we will follow NAR safety rules and regulations. ► We will follow standard.
The Rocket Men Project One Giant Leap. Final Launch Vehicle Dimensions Rocket Length in. Rocket Mass- 171 oz. Top Body Tube Length in. Bottom.
Flight Readiness Review Student Launch Initiative SCS Rocket Team Statesville Christian School April 2, 2008.
NASA SLI 2010 Mulberry Grove High School Flight Readiness Review Measurement of UVB Radiation Absorption by Cloth Material at Different Altitudes and Measurement.
FRR Presentation IF AT FIRST YOU DON’T SUCCEED, TRY AGAIN… AND AGAIN AND AGAIN AND AGAIN.
D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB PDR PRESENTATION 1.
Flight Readiness Review “Analysis of Atmospheric gamma radiation as a Function of Altitude by means of Scintillator Probe” St. Thomas High School, Houston,
ROCKET Done by, ARDHRA P.B. & RAMYA D. Standard : X Govt. Girls Higher Secondary School, Pattom, Trivandrum.
Student Launch Project Critical Design Review February 28, 2014.
Seattle Central Community College, Seattle, Washington Science and Math Department Members: Colin Webb, Cooper Clausen, Luan Duong, Brian Injugu.
Preliminary Design Review “Analysis of Atmospheric Cosmic Radiation Distribution as a Function of Altitude” Steven Schroeder-Program Manager Damon Emerson-Rocket.
FAMU PDR Presentation. Table of Contents Vehicle dimensions, materials, and justifications Static stability margin Plan for vehicle safety verification.
Bellerophon 1kg Exploded View Sarah Shoemaker. Spin Table 3 rd Stage Engine 2 nd Stage Avionics 2 nd Stage Engine 2 nd Stage Propellant Tank 2 nd Stage.
CDR Clear Lake's Team Rocket 2929 Bay Area Blvd. Houston, TX
Launch Vehicle Launch Vehicle Summary The length of the rocked is inches, and the mass is ounces. We have a dual Deployment Recovery.
NUSTA RS NASA Student Launch MAV Challenge 2016 Critical Design Review 15 Janurary2015 Northwestern University | 2145 Sheridan Road | Evanston, IL
January 14, Length: inches Diameter: 6 inches Mass: oz. / lbs. Span: 22 inches Center of Gravity: inches
Student Launch Project Flight Readiness Review April 21, 2014.
NASA CDR Presentation Spring Grove Area High School.
University of Florida PDR Presentation. Vehicle Design Diameter: 5.86 Length: 135 Static Stability Margin: 1.4 Total Weight: 23.6 lbs.
Critical Design Review ….. Royal Ordnance,Summerfield 17 th February 2001 National Rocketry Competition 2001 Open Rocketry Association Slide 1/14.
Launch Vehicle Propulsion Payload Recovery Vehicle Dimensions Total length of inches 4.0” Airframe (3.9” Inside diameter) Fin span of 3.91” Separates.
Preliminary Design Review “The Distribution of Ionizing Radiation with Altitude” Left to Right: Tom L.- Payload James Z.-Construction Izzy S.- Audio Visual.
University of Arkansas Senior Project- When Pigs Soar.
Preliminary Design Review Clear Lake High School Team Rocket.
Page 1 TESLA Rocket Project Lecture #3 10/28/15. Page 2 1)Critical Path Activities 2)TESLA Rocket Overview & Other Stuff 3)Next Week Evening Session?
NUSTA RS NASA Student Launch MAV Challenge 2016 Preliminary Design Review 6 November 2015 Northwestern University | 2145 Sheridan Road | Evanston, IL
All teams are provided with a “kit” – set of (mostly cardboard) templates to assist with rocket assembly Our kit will be a “North Star” design seen.
University of Florida Rocket Team Critical Design Review Presentation.
Page 1 Recovery Discussion 11/4/2015. Page 2 Roles & Responsibilities ? Point Of ContactResponsibility Alisson Clark Liam Jaffe Yash Pahade Yumi Shridhar.
P RELIMINARY D ESIGN R EVIEW University of North Dakota Frozen Fury Rockety Team.
Hemodynamics Star Splitters 4-H Club Two Rivers, WI Hemodynamics.
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.
Critical Design Review “The Distribution of Ionizing Radiation with Altitude” Left to Right: Izzy S.- Audio Visual Tom L.- Payload James Z.-Construction.
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