Century College Digital Fabrications Lab White Bear Lake, Minnesota Fab9 Yokohama August 21, 2013.

Slides:



Advertisements
Similar presentations
PANTHR Hybrid Rocket Final Design Review December 6 th 2006.
Advertisements

Preliminary Design Review. Rocket & Payload Schematic.
Northwestern University Space Technology and Rocketry Society (NUSTARS) NASA Student Launch Flight Readiness Review March 16, 2015.
Eddie McGovern, Adam Blake, Ryan Vogel, Alleyce Watts, and Jade O’Mara.
Critical Design Review NASA University Student Launch Initiative University of Nebraska–Lincoln
Student Launch Project Preliminary Design Review January 10, 2014.
U NIVERSITY OF F LORIDA I NTIMI GATOR PDR. O UTLINE Project Organization Vehicle Design Payload Design Recovery System Component Testing Subscale Flight.
U NIVERSITY OF F LORIDA PDR P RESENTATION. O UTLINE Project Organization Vehicle Design Payload Design Recovery System Simulations Future Work.
Project Λscension. Vehicle Dimensions Weight: 19.6 Ib Length: in (9 ft. 4.5 in) Diameter: 6 in Fin Semi-Span: 6 in.
St. Vincent – St. Mary CDR Presentation NASA Student Launch Initiative.
St. Vincent – St. Mary FRR Presentation NASA Student Launch Initiative.
UAA Rocketry Critical Design Review Presentation.
NASA SLI 2010 Mulberry Grove High School Flight Readiness Review Measurement of UVB Radiation Absorption by Cloth Material at Different Altitudes and Measurement.
Windward Community College. Rocket: Leo Hano Payload: Hula-hoop.
Student Launch Project Critical Design Review February 28, 2014.
Hawaii - WCC.  5,280 ft  Carry a student payload  National CanSat program  No bigger than a 12 fl oz soda can  Mass no greater than 1 kg  USLI.
Critical Design Review. Intimidator 5: 5” diameter, 10’ length, 45 lbs  Motor: Aerotech L1300R 4556 N-Sec of impulse  Predicted altitude RockSim.
Flight Readiness Review Atomic Aggies. Final Launch Vehicle Dimensions Diameter 5.5” Overall length: inches Approximate Loaded Weight: lb.
CDR Clear Lake's Team Rocket 2929 Bay Area Blvd. Houston, TX
Intercollegiate Rocket Engineering Competition Spring 2015 EML Ethics and Design Project Organization.
Rocket Based Deployable Data Network University of New Hampshire Rocket Cats Collin Huston, Brian Gray, Joe Paulo, Shane Hedlund, Sheldon McKinley, Fred.
Tropos-1 Hybrid rocket Project
CanSat Concept Generation
Launch Vehicle Summary Rocket Name: The Green Machine 124 inches in length 6” diameter L1500T 98-mm motor 42” drogue deployed at apogee 144” main to be.
 Vehicle dimensions, materials, and justifications  Static stability margin  Plan for vehicle safety verification and testing  Baseline motor selection.
Windward Community College University of Hawaii
Flight Readiness Review Team Hawaii. Vehicle Properties Diameter (in)6 inches Length (in)127 inches Gross Liftoff Weight (lb)50.25 lb Launch Lug/button.
The Rocket Men Project One Giant Leap. Final Launch Vehicle Dimensions Rocket Length in. Rocket Mass- 171 oz. Top Body Tube Length in. Bottom.
University of Arkansas Senior Project- When Pigs Soar.
STUDENT LAUNCH PRELIMINARY DESIGN REVIEW PROJECT ADVANCE.
FRR Presentation IF AT FIRST YOU DON’T SUCCEED, TRY AGAIN… AND AGAIN AND AGAIN AND AGAIN.
Windward Community College University of Hawaii
University of Florida Rocket Team Critical Design Review Presentation.
AAE 450 Spring 2008 Tim Lorenzana 1/16/2008 Avionics Recovery/Termination.
Vanderbilt Aerospace Club Rocket Launched Reconnaissance UAV Design Team William Runge (ME) Kyser Miree (ME) Thomas Carroll (ME) Thomas Bowden.
University of Arkansas Senior Project- When Pigs Soar.
Critical Design Review- UCF Jeremy Young Anthony Liauppa Erica Terry, Emily Sachs Kristen Brightwell Gillian Smith 1.
M E T ROVER MSCD Engineering Technology Critical Design Review Metropolitan State College of Denver April 2004.
WINDWARD COMMUNITY COLLEGE UNIVERSITY OF HAWAII
Can - SAT Project. Agenda Project Description CanSat Objectives Project Objectives Project Rules –Mandatory –Optional History of CanSAT Design Goals Team.
Introduction & Overview
Atomic Aggies CDR. Final Launch Vehicle Dimensions Diameter 5.5” Overall length: inches Approximate Loaded Weight: lb.
High Altitude Balloon Michael Adams Alex Fletcher Jon Welch.
Flight Readiness Review “Analysis of Atmospheric gamma radiation as a Function of Altitude by means of Scintillator Probe” St. Thomas High School, Houston,
Project Ares University of Central Florida NASA Student Launch 1/28/2015.
D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB PDR PRESENTATION 1.
TESLA Rocket Project Lecture #3 10/28/15
University Student Launch Initiative Team Members Todd Esposito Patrick Lancaster Joleen Iwaniec Premo Ames II Jazmine Maru Jazmine Maru.
HARDING UNIVERSITY FLYING BISONS A Study of Atmospheric Properties as a Function of Altitude Flight Readiness Review.
University Student Launch Initiative Preliminary Design Review University of Illinois at Urbana-Champaign Team Rocket.
January 14,  Length: inches  Diameter: 6 inches  Mass: oz. / lbs.  Span: 22 inches  Center of Gravity: inches 
Page 1 TESLA Rocket Project 11/4/15. Page 2 1)Schedule 2)Launch Performance & other stuff.
Critical Design Review Presentation Project Nova.
Flight Readiness Review UNIVERSITY OF SOUTH ALABAMA CONNER DENTON, JOHN FAULK, NGHIA HUYNH, KENT LINO, PHILLIP RUSCHMYER, & ANDREW TINDELL MENTOR : RICHARD.
Jump Vehicle Details Ping Pong Productions. Design Strategy Start with an already proven vehicle concept Improve upon it with modern technology Allow.
UCF_USLI Preliminary Design Review David Cousin Freya Ford Md Arif Drew Dieckmann Stephen Hirst Mitra Mossaddad University of Central Florida.
Preliminary Design Review Presentation
Preliminary Design review
Critical Design Review Presentation
2018 First Nation Launch - Flight Readiness Review
NASA USLI Preliminary Design Review
Century College-Fab Lab
Final Readiness Review
2019 First Nation Launch – FRR Virtual Review
2019 First Nation Launch – PDR Virtual Review
Windward Community College ARLISS/USLI Presentation Fall 2009 KCC, Ohi’a Room 118 November 21, 2009 Premo Ames II Todd Esposito Joleen Iwaniec Patrick.
2019 First Nation Launch – Oral Presentation
Characteristics,Construction, Recovery
University of Iowa USLI
2019 First Nation Launch – Oral Presentation
Presentation transcript:

Century College Digital Fabrications Lab White Bear Lake, Minnesota Fab9 Yokohama August 21, 2013

NASA Rocket Competition Project

-NASA STUDENT LAUNCH INITIATIVE -40 COLLEGES -ROCKET TO ACHIEVE 5280 FEET (EXACTLY) -ROCKET PAYLOAD (ROVER) -A ONE YEAR PROJECT Funded by Century College Foundation ($10,000)

THE COMPUTER AIDED ROCKET DESIGN

FABRICATION

THE TEAM SARA LAWSONTEAM LEAD KEITH KOPPENAIRFRAME CHRISTOPHER PEPINELECTRONICS JACOB VOGESELECTRONICS/SAFETY SAM COURTIERAPPLIED MATHEMATICS JEFF RANDALLCAD – ROVER DESIGN TODD HANSONROVER GOKHAN SARIRECOVERY JOHN RUPERTTEAM ADVISOR GARY STROICKTEAM MENTOR

Drag Brake Design The CFX-12's drag brake, is a retractable nose cone that will allow us to control our maximum altitude.

Rover Design The rover is an autonomous vehicle capable of maneuvering on its own using GPS Navigation –Wheel diameter: 5 in. –Length: 10 in. –Weight: 5lbs

RECOVERY SYSTEM RECOVERY SYSTEMS USES DROGUE CHUTE AND MAIN CHUTE TO MINIMIZE DRIFT AND IMPACT VELOCIY

ELECTRONICS DRAG BRAKE ELECTRONICS TWO MICROCONTROLLERS TELEMETERY SENSORS 7 ACCELS GPS ALTIMETER PROX SENSOR ACTUATORS DC MOTOR FOR BRAKE DEPLOYMENT ROVER ELECTRONICS ONE MICROCONTROLLER TELEMETERY SENSORS GPS MAGNETOMETER ACCELEROMETER ACTUATORS 2 DC MOTORS ARRD

TEST PROGRAM 2 STRING TESTSSTABILITY 5 HALF SCALE FLIGHT TESTS #1ELECTRONICS, BRAKE, 1RST #2TELEMETRY #3HIGH DATA RATE TELEMETRY #4MASS PROPERTIES - BALLAST #5STABILITY, FULL SCALE ELECTRONICS 1 WIND TUNNEL TESTSTABILITY, BRAKE Cd 2 EXPULSION TESTSMAIN, DROGUE/ROVER 1 FULL SCALE LAUNCHSTABILITY, BRAKE Cd, FS ELECTRONICS 2 ND FULL SCALE LAUNCHTARGET ALTITUDE CONTROL, RECOVERY NASA MSFC LAUNCHWIN! TEST OBJECTIVES

TEST RESULTS STATISTICS FLIGHT TEST DATA: WIND TUNNEL TEST DATA: ODE & NON LINEAR REGRESSION DRAG COEFFICIENT – NON LINEAR REGRESSION BRAKE CONTROL ALGORITHM - NEWTON’S LAWS

EDUCATIONAL ROLE OF PROJECT PROJECT BASED (HANDS ON) LEARNING FOR ENGINEERING STATICS DYNAMICS DEFORMATION OF MATERIALS CIRCUITS ROBOTICS APPLIED MATHEMATICS: STATISTICS ODE PROGRAM MANAGEMENT A THESIS LEVEL PROJECT OF ONE YEAR DURATION FOR IN DEPTH EXPOSURE TO ADVANCED TECHNOLOGY

Prototype to Market-Slatgrill.com

Minnesota Fab Lab- in Process Duluth Public Schools-Duluth Minnesota Saint Paul Public Schools Stillwater High School Lake Superior College, Duluth Minnesota White Bear Lake High School District 914 Eagan Minnesota Elk River School District, Elk River Minnesota Others…..

Planning -Hire 2 Fab Lab Technicians -Design and Construct New Fab Lab -Expand STEM Focus -Become Minnesota’s STEM Resource Center -Develop New Engineering Degree Digital Engineering -Develop Partnership with Workforce Minnesota -Continue assisting New Fab Labs in Minnesota