Kevin Dahya Critical Design Review 3/6/01

Slides:



Advertisements
Similar presentations
2E4: SOLIDS & STRUCTURES Lecture 8
Advertisements

Check Beam Shear.
Structural Mechanics 6 REACTIONS, SFD,BMD – with UDL’s
Lecture 9 - Flexure June 20, 2003 CVEN 444.
SHEAR IN BEAMS. SHEAR IN BEAMS Example (4.1): A rectangular beam has the dimensions shown in Figure 4.12.a and is loaded with a 40 ton concentrated.
Chp.12 Cont. – Examples to design Footings
PROJECT 100. PROJECT 100 DESIGNED TO BE: Cost Effective Compact Strong Simple Light Reliable.
DETAILED DESIGN REVIEW NOVEMBER 11, 2011 MSD I HUMANOID ROBOT P12201.
THE WASHINGTON MONUMENT (1884) The purpose of this study is to show how this structure supports its own weight and wind load, by calculating its efficiency.
ME221Lecture 281 ME 221 Statics Lecture #28 Section 7.4.
AAE450 Senior Spacecraft Design Project Aquarius Kowalkowski - 1 Mike Kowalkowski Week 11: April 5 th 2007 Project Aquarius Final Presentation Storyboard.
DEFLECTIONS (Chapter 8) WHY? FACTORS IN DESIGN Safety Esthetics Serviceability Environment Economy DETERMINACY Determinate Structures Equations of Equilibrium.
ENGR 220 Section 6.1~6.2 BENDING.
AAE 450 – Spacecraft Design 1 Mars Entry Aerodynamic Design Mark W. Vahle 18 January 2005 Aerodynamics Team Also working with Propulsion, Thermal, and.
Structure Analysis I. Lecture 8 Internal Loading Developed in Structural Members Shear & Moment diagram Ch.4 in text book.
ME 501 Corey Roberts Leo Montgomery Motor Plate Analysis.
Missouri City, TX TV Antenna Collapse 1985 Based on Texas A&M engineering ethics web site.
AAE450 Senior Spacecraft Design Atul Kumar Presentation Week 3: February 1 st, 2007 Aerodynamics Team Re-Entry vehicle analysis - Lifting body 1.
ME221Lecture 271 ME 221 Statics Lecture #27 Section 7.4.
ME221Lecture 151 ME 221 Statics Lecture #15a Sections
AAE450 Senior Spacecraft Design Brandon Anderson Week 3: February 1st, 2007 Structures Group Taxi Capsule, Electric Propulsion System.
Copyright © 2011 Pearson Education South Asia Pte Ltd
Reinforced Concrete Design II
Minimum Weight Wing Design for a Utility Type Aircraft MIDDLE EAST TECHNICAL UNIVERSITY AE 462 – Aerospace Structures Design DESIGN TEAM : Osman Erdem.
Chapter 4 - Flexure. Lecture Goals Structures Basic Concepts Rectangular Beams.
Factor of Safety (Safety Factor) In the calculations, Material strengths, Manufacturing process Is used to provide a design margin over the theoretical.
British Space Service Astronaut Test Paper 1 (Trip to Mars)
Proper lifting techniques
AAE 450- Propulsion LV Stephen Hanna Critical Design Review 02/27/01.
Mars Today 1 An immediate and inexpensive program for manned Mars visitation.
Structural Design for Cold Region Engineering Lecture 14 Thory of Plates Shunji Kanie.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
AAE450 Spring 2009 Primary structure for Orbital Transfer Vehicle (OTV) Tim Rebold STRC [Tim Rebold] [STRC]
Gravity and Center of Gravity. What do you know about gravity? Gravity is a force that pulls things together based on there mass and how close they are.
Forging new generations of engineers
Chapter 11 Design of Beams (Sections 1 and 2). Recall, with beams we have two stresses to deal with, normal stress, , and shear stress, 
Sam Krueger.  Entertainment Center  Preliminary design  Initial  36 plies, glass epoxy  [0 11 /±45 1 /90 5 ] s  No core  Modified design  36 plies,
A&AE 450 – Senior Design Jeremy Davis Group A – Aerodynamics Preliminary Design Analysis January 23, 2001.
Structures PDR 1 Team Boiler Xpress Oneeb Bhutta Matthew Basiletti Ryan Beech Micheal VanMeter October 12, 2000.
AAE450 Senior Spacecraft Design Atul Kumar Week 1: January 18 th, 2007 Aerodynamics Team Entry vehicle analysis 1.
LHCb Radiation Shielding Wall – Lifting Tool Overview.
ILC Dover Proprietary Information “Z” Suits” NASA’s Exploration Extravehicular Activity Space Suit Development Program FISO Telecon Phil Spampinato.
Beam Design Beams are designed to safely support the design loads.
ERV Team 2 Final Report Alicia Cole-Quigley James Gilson Erin Hammond Domenic Marcello Matt Miller Jeff Rosenberger.
AAE450 Senior Spacecraft Design Kate Mitchell Week 2: January 25 th, 2007 Human Factors – Team Lead Habitat (HAB), Crew Transfer Vehicle (CTV) This Week:
Main Steps of Beam Bending Analysis Step 1 – Find Reactions at External Supports –Free Body Diagram (FBD) of Entire Beam –Equations of Force and Moment.
An Earth – Moon Transportation System Patrick Zeitouni Space Technology.
Preventing Back Injuries 10 80% Have Back Pain 80% Have Back Pain 9.
AAE450 Spring 2009 Lander Sizing and Launch Vibrations Feb. 12, 2009 Earth Launch/Lunar Descent Phase Group 1 [Ryan Nelson] [STRC]
A&AE 450 – Senior Design Avionics March 6, 2001 Wiyan Wong.
TOPIC 3: DESIGN AND ANALYSIS OF SHALLOW FOUNDATION
SAE Aero 2017 Midterm Presentation Joe Zongolowicz, Nick Montana, Frank Dixon, Kevin Scheventer, Kathy Hansen, Marquis Ward, Gerald Short, Zhangsiwen Xiao,
An-Najah National University Faculty of Engineering
Tilt N’ Store Design Analysis
1. Launch Mother Ship to LEO
Structures and Weights 1 QDR
What is Transportation?
In-situ Propellant Production and ERV Propulsion System
Structures and Weights Preliminary Design Review
Back Safety: Lifting Odd Shapes
ERV Design Chris Heidelberger Dynamics & Control
KEVIN DAHYA STRUCTURES – ERV
Structure Analysis I Eng. Tamer Eshtawi.
AAE 450- Propulsion LV Stephen Hanna Design Review 02/19/01.
Brandon Abel – Human Factors
Structures and Mechanisms
Team 5 Structures and Weights QDR #1
Jayme Zott Aerothermodynamics Aerodynamic Loads Special thanks to Alex Woods, CJ Hiu and the entire trajectory group AAE 450 Spring 2008.
Forging new generations of engineers
STRUCTURES & WEIGHTS QDR 1
Presentation transcript:

Kevin Dahya Critical Design Review 3/6/01 Structures-ERV Kevin Dahya Critical Design Review 3/6/01

Launch off Earth ~ 85.8 Tonnes Landing on Mars ~ 55.2 Tonnes KEVIN DAHYA Weights Launch off Earth ~ 85.8 Tonnes Landing on Mars ~ 55.2 Tonnes Launch off Mars ~ 10 Tonnes Return to Earth ~ 5 Tonnes

KEVIN DAHYA Shape

KEVIN DAHYA Inside Layout

KEVIN DAHYA Dimensions Sizing Breakdown Crew Quarters ~300m3 Propulsion/ In-Situ Plant / Power Plant ~650m3 Rover Garage ~200m3

KEVIN DAHYA CTV

Lifting Body for better L/D Used for entry into Earth atmosphere KEVIN DAHYA CTV Lifting Body for better L/D Used for entry into Earth atmosphere Space for Crew and necessities Can be used for 0 abort on Mars

KEVIN DAHYA CTV - Dimensions

KEVIN DAHYA Bending Loads (Aerobraking) Wrote Matlab Code Calculated for 6g loading Bending Analysis by Sections Gives Shear and Moments Assumes 3 point bending Found Max Bending Stress Margin of Safety > 0 MS = 0.5

KEVIN DAHYA Things to do Layout of ERV (Crew Living Area) Landing Loads and Landing Leg Design Propulsion Layout Weights !!! Build