T roops I n C ontact R esupply Team Cougar Anthony Brock Henry Goodell Nathan Lambert Patrick Fain Eric Fleischhauer James Haig.

Slides:



Advertisements
Similar presentations
Business Process Reengineering Raymond Yap Principal Consultant Hutex Management Consulting
Advertisements

Design of spur gear transmission
Federal Aviation Administration On-Orbit Debris Mitigation Methods for Upper Stages COMSTAC: Space Transportation Operations Working Group and Risk Management.
High Altitude Balloon Instrument Survival Package Joseph Burns, Tom Fox, Austin Isitor, Nick Schuyler.
A Sled System for Motor Vehicle Crash Simulation and Forensic Biomechanics Group Members: Joshua Booren Travis Deason Steve Savas Max Brunhart Customer:
Teaching materials to accompany:
Team Rocket Sled Team: Tom BartoskiBrian BitterBrian Dearolf Robert GiffordTom Koehler Customers: Dave Scott Advisor: Dr. Len Schwartz Jack Armstrong.
Design Review Three Micro Air Vehicle Project: P Sponsored by Impact Technologies The Boeing Company Mark Baybutt Electrical Engineering.
AAE 451 SPRING 2007 SYSTEMS REQUIREMENTS REVIEW TEAM 4: Kevin Kwan Dan Pothala Mohammad A. Rahim Nicole Risley Sara Tassan John Thornton Sean Woock Alvin.
Ken Youssefi Introduction to Engineering – E10 1 Design Process Concurrent Engineering.
Strategic cost analysis 2
Teaching materials to accompany:
CE 353 Lab 7: Rail Design Part 1: Train Acceleration, deceleration, and impact on Capacity Part 2: Design of a hump yard / classification facility Initial.
Intercollegiate Rocket Engineering Competition Spring 2015 EML Ethics and Design Project Organization.
Nonaxial Wind Turbines A New Class of Wind Turbines By Mike Fallwell.
Lecture 2 Engineering Design Process & Method. Introduction Design is a multidisciplinary field which integrates the scientific principle, technical information.
Definition of Concurrent Engineering "Concurrent engineering is a systematic approach to the integrated, concurrent design of products and their related.
How can simulation boost the industry productivity in design and innovation stages ? Cécile Goffaux Energy & Buildings Team Leader at Cenaero
MIT ICAT MIT ICAT 1October 17, 2002 Exploring the Envelope of a Modified 3° Decelerating Approach for Noise Abatement Liling Ren & John-Paul Clarke October.
Aircraft of Vietnam By Justin Pinca. Thesis: Many aircraft advancements were based on the conditions of the Vietnam War.
University of Arkansas Senior Project- When Pigs Soar.
Work IN, Work OUT The Work/Energy Principle. Kinetic Energy KE depends on mass and velocity Work done on an object will change KE.
Ken Youssefi Mechanical Engineering department 1 Design Process Concurrent Engineering.
In most situations, at least two forces act on any object. The overall effect of these forces makes it act differently. For example, if a falling object.
Part 1 Gravity and Free Fall Free Fall An object is in free fall if it is accelerating due to the force of gravity and no other forces are acting on.
2011 Human Powered Vehicle Challenge 'Mjolnir' Team Members: Tad Bamford Ben Higgins Chris Schultz Aaron Stanton Neal Pang.
Projectile Kinetic Energy Reduction System (PKERS)
Formula SAE Flow Testing Device
Ken Youssefi Mechanical Engineering department 1 Introduction to Concurrent Engineering Computer Aided Design (CAD) Computer Aided Manufacturing (CAM)
Chapter 12 EIN 6392, Product Design summer 2012
The Engineering Design Process
P07108: METEOR Instrumentation Recovery System. Team Bash Nanayakkara – Project Manager (ISE) Scott Defisher – Fuselage Design (ME) Mike Kochanski – Software.
Chapter 5 Outline Applying Newton’s Laws Statics Dynamics Friction Static friction Kinetic friction Fluid resistance Circular Motion Fundamental forces.
Concurrent engineering By: Reza VATANKHAH. Field warranty service Production system Prototyping Process design GD&T Quality control Product design GD&T.
Recommendation to Cease NASA Crew Return Vehicle Development April 29, 2004 Amanda KellyBlake HajovskyAnthony Pittman Engineering Technical Communications.
6 Modeling, Testing, and Final Outputs Permission granted to reproduce for educational use only.© Goodheart-Willcox Co., Inc. Objectives Explain the.
Breaking Contact B Trp 7-10 CAV 4ID Reference Material
COSMOS DRONES. Art & Drones mix the most futuristic technology scenarios with our aerial hoop drone performances, known as Cosmos Drones See the video.
Constructing your own landing device An exploration into the elementary physics behind the landing of the Mars rover and Apollo space capsules.
4A6 CASE STUDY PRESENTAION World Trade Centre Collapse.
E8: Digital Humans Option E AHL: Human Factors Design IB Technology.
Design Process Concurrent Engineering
Auto Tow Conversion Course
1-2-4 Horizontal Projectiles
Sustainable/Green IT Practices
Midstream Natural Gas Impurities Measurement
Airfoil Any surface that provides aerodynamic force through interaction with moving air Aerodynamic force (lift) Moving air Airfoil.
Zeppelins By: Tony”Big toe” A., Liza , Jimmer_10,Kayla”K-money” , & Erin McChicken.
Date of download: 11/16/2017 Copyright © ASME. All rights reserved.
Top Cabin Crew Job in India by Airwing Aviation Academy india.aspx Address: First Floor,
Please highlight one choice only
Modern Graphics Communication
[insert category name] [insert date]
Topic 3 Modeling.
Engineering Design Process
Assessing Risk Impact Factors affecting the consequences Nature Scope
Aim: How do we solve complicated projectile motion problems?
Trials - Historically a Success
1-2-4 Horizontal Projectiles
AS Apply a design process and design principles to identified needs and opportunities Sample 1. Merit.
Please highlight one choice only
1-2-4 Horizontal Projectiles
Aim: How do we solve complicated projectile motion problems?
Maintenance Opportunities
Chapter 12 EIN 6392, Product Design Fall 2009
University of Iowa USLI
Chapter 2: Development process and organizations
Extreme Altitude Mountain Rescue Vehicle
TEAM NAME: VERSION 2 MODEL TEST 1
Presentation transcript:

T roops I n C ontact R esupply Team Cougar Anthony Brock Henry Goodell Nathan Lambert Patrick Fain Eric Fleischhauer James Haig

Concept of Operation Troops in sustained contact run low on ammunition. Due to sustained adversarial small arms fire, RPG usage, and crew served weapons, the risk of aircraft loss is high during traditional helicopter resupply. This is due to the need to reduce speed to 40 knots and reduce altitude to below 40 ft. Using additive manufacturing to produce a drop capsule with a structure designed to absorb impact that can only be made through 3D printing, we can mitigate the risk to aircraft and personnel by allowing resupply from aircraft at 150 ft at 90 knots. This greatly reduces the aircraft profile and amount of time that aircraft are presented as targets of opportunity.

Toroidal Parachute Reusable Top Section Internal Supplies Disposable Impact Section

TICR system advantages Structure custom 3D printed for: type of supply, mission, impact Made with biodegradable PLA FDM for “leave behind” disposability Parachute slows TICR to safer speed from safe helicopter altitude

Math Dropped from 150ft from a helicopter going 90 knots Results in an unresisted final velocity of approximately 124 mph This would need to be adjusted for air resistance For a 35 pound load the impact energy is 17,800 lbf-ft (from final kinetic energy at 124 mph) This information can be used to help model what strength the collapse structure would need to have

Impact Stage Lattice Structure

Design process Problem Identification Feasibility Analysis Initial CAD design using circular crush structure Structure refinement and hexagonal implementation Prototype CAD designed finalized Prototype design printed

Future Development Explore alternate print techniques Refine design structure Experiment with alternate print materials Finite element analysis & computation fluid dynamics Drop testing and iteration Safety Analysis