Juggernaut Team 3 Completed Design Review Becca Arvanites: Structural Design Mark Egan: Structural Analysis & Stability Karl Kulling: RC Operator/communications.

Slides:



Advertisements
Similar presentations
Click to Add Title CDR: Spring, The Team Alex Coso Fred Gay Dan Cunningham Val Lugo.
Advertisements

 A radio controlled aircraft (model) is controlled remotely by a hand held transmitter & receiver within the aircraft.  The.
Force Diagrams and Calculations More Math!!!. Force Diagram 1 Are the forces acting on this object balanced or unbalanced? What is the net force acting.
Giving Bertha! LTA CDR David Dryjanski – Design/Construction, SolidWorks Expert Rachel Ellman - Design/Construction Carl Engel - Team manager, Propulsion.
Find and simplify g(x+1) Answer:. Evaluate f(-1) Answer:
Drag Queen LTA Completed Design Review Nestor Lara, 2004.
Guidelines Presentation. Aircraft Aim & Judging The aircraft needs to transport the mirror segments of the ESO European Extremely Large Telescope, being.
1. P09203 – 1kg Robotic Motor Module Gen 2 Platform This project is Sponsored by the Kate Gleason Foundation.  Team Members:  Lauren Farnsworth → Team.
1. P09203 – 1kg Robotic Motor Module Gen 2 Platform This project is Sponsored by the Kate Gleason Foundation.  Team Members:  Lauren Farnsworth → Team.
Group 2 Sunny Wicks, Rebecca Sampson, Nikki Akraboff, Ellis Langford, Garret Crandall.
Completed Design Review Team Airblade Timothy Davenport Brian Guerrero Mark Kastantin Oscar Kataura William Peters Robert Taylor.
BELIEVE. Lighter Than Air Vehicle Completed Design Review Team Two “Believe”
Vehicle Sizing PDR Presented by: Mark Blanton Chris Curtis Loren Garrison September 21, 2000 Chris Peters Jeff Rodrian DR2.
AAE 450 – Spacecraft Design 1 Mars Entry Aerodynamic Design Mark W. Vahle 18 January 2005 Aerodynamics Team Also working with Propulsion, Thermal, and.
4 Spheres 3 Presents The Development of Gus™. Objectives  Reliability, stability and controllability  Most efficient battery usage possible  Clarify.
Lighter Than Air Critical Design Review Mark Cote Yonas Tesfaye Josh Levinger Bryan Owens The A-Team.
DR2 Propulsion PDR I Preliminary Design Review II October 17, 2000 Presented By: Mark Blanton Team DR2 Chris Curtis Loren Garrison Chris Peters Jeff Rodrian.
Critical Design Review The Fab Four Jeremy Conrad Jeremy Conrad Electronics Expert Electronics Expert Javier Matamoros Javier Matamoros Thrust Guru Thrust.
Team Weatherman Completed Design Review James Banks, Test Engineer Katonio Butler, Electrical Specialist Alex Cutting, Structural Engineer Lori Huberman,
Barry Barrios Structural Engineer Daniel Chaparro Structural Engineer Laura Garrity Propulsion Chad Lieberman Control Surfaces Adam Vaccaro Electrical.
The Four Forces of Flight
GENERAL DESCRIPTION An airplane or aeroplane (informally plane) is a powered, fixed-wing aircraft that is propelled forward by thrust from a jet engine.
THE INVENTION OF THE AIRPLANE ORVILLE WILBUR Part 1: Background & Failures.
ELEMENTS OF AEROSPACE ENGINEERING AND DESIGN ENME 489L Fall Aerodynamic Analysis 3 Balloons in straight line Maximum Lift Minimum Drag.
Quiz 4.
1.) An object projected straight upward with an initial velocity of 88.2m/s will reach its maximum altitude of 396.9m in 9s. If after 5s the object is.
Aircraft Familiarization
Miguel Jimenez Ricardo Lugo Carlos Rojas Advisor: Andres Tremante.
1) If drag is 26,400 N and the lift is 29,300 N, determine the weight, mass and thrust, given that the plane is traveling at a constant velocity. What.
Newton’s 2 nd Law. Get a whiteboard & a marker! You may work with a partner or by yourself! Have your NB open to pg. 20 & write “WB’s” at the top! You’ll.
ES 100 Micro Air Vehicle Project Montgomery College Professor: Dr. Charles Kung Summer I 2012 Team Members: Andrew Joe Laura Mohammed Nathelie Noella Stephanie.
Accelerated Motion. is changing either the speed or direction, or both, of motion. Acceleration is the rate of change of velocity, in other words, how.
DR2 Propulsion PDR I Preliminary Design Review September 28, 2000 Presented By: Mark Blanton Team DR2 Chris Curtis Loren Garrison Chris Peters Jeff Rodrian.
10/25 Momentum in 2D  Text: Chapter7  HW: HW Handout “Pendulum and Block” Due Wednesday, 10/30  HW Questions?  Examples.
Newton’s Second Law of Motion. 2 nd Law of Motion  The net (total) force of an object is equal to the product of its acceleration and its mass.  Force.
DR1 PF, E, & FTP PDR Prototype Fabrication, Economic and Flight Test Plan Preliminary Design Review October 26, 2000 Presented By: Mark Blanton & Chris.
F = ma F = Force m = Mass a = Acceleration. The Manned Manoeuvring Unit.
Uncontrolled copy not subject to amendment Rocketry Revision 1.00.
Critical Design Review Team Floating Point MIT April 25, 2003.
Yaqoub Almounes John Cowan Josh Gomez Michael Medulla Mohammad Qasem
Newton’s Laws Practice
Chapter 4-3 Newton’s 2nd and 3rd Laws.
Balanced and Unbalanced Forces
How An Airplane Flies by Fernando Salas PBL
Four Forces of Flight Lift Weight Thrust Drag
Newton’s 2nd Law Put on pg.20 in NB.
Do now A baseball player holds a bat loosely and bunts a ball. Express your understanding of momentum conservation by filling in the tables below.
Review for Quiz What is the formula for speed?
Newton’s First and Second Laws
Notes 2.2: Newton’s 2nd Law of Motion
Motorized Antenna Mount
Find the velocity of a particle with the given position function
stages control devices thrust arrangement
Alfred Lynam February 7, 2008 Dynamics and Control Architecture of Control System: Controller Prototypes AAE 450 Spring 2008 Dynamics and Control.
100 g Locomotion Thursday March 26, Ryan Lehto Propulsion Group
Development and Principles of Rocketry
Momentum.
Find the velocity of a particle with the given position function
Calculations and Worked Examples
Circular Motion What is acceleration?
This waveform is 35.0 cm long. How long is the wavelength?
Theory of Flight Forces of Flight MS-PS2-2.
Rocket Problems Answers
Do now A baseball player holds a bat loosely and bunts a ball. Express your understanding of momentum conservation by filling in the tables below.
Net Force Contents: What is the Net force
AP Forces Review Problem Set Answers
Jumping from a Cart Competition sp 4, page 248
Motion & Forces: Newton’s Laws of Motion
Jeff Stuart 2/28/2008 Dynamics and Controls, CAD Spin Stabilization of Third Stage (200g Payload) AAE 450 Spring 2008.
Mass and Motion.
Presentation transcript:

Juggernaut Team 3 Completed Design Review Becca Arvanites: Structural Design Mark Egan: Structural Analysis & Stability Karl Kulling: RC Operator/communications & Propulsion Chris Savage: Stability & Structural Design Dawn Wheeler: Propulsion & RC Communications

Why a Four-Balloon Diamond Design? Benefits:  Advantageous payload  Stability in all directions  Vectored Thrust

Control Systems  Vectored Thrust: one servo controls pitch of motors, another servo controls yaw of motors  RC control (human factors)

Aerodynamic Analysis  Maximum Thrust (from table): 1.4N total from 2 large motors  Mass: kg  Maximum Acceleration = Thrust/Mass =.9-1m/s 2  Terminal Velocity = m/s  Time Estimate: seconds

Design Evolution  Reshaping control assembly to allow room for propellers to turn  Motors mounted under control assembly instead of on top  Extra bracing required on control assembly  Psychological evolution: new improved team name! <-- motor mount prototype

Conclusions  Designed for stability and payload rather than aerodynamics/speed  Building left: attach motor mount to fuselage, balloon attachment net  Testing: controls response, practice using rc controller