1 Formation Flying Project Proposal 2/5/07 Rachel Winters (Team Lead) Aziatun Burhan Tsutomu Hasegawa Shunsuke Hirayama Matt Mueller Masao Shimada Shelby.

Slides:



Advertisements
Similar presentations
Unit 3, Chapter 9, Lesson 9: Space Systems Engineering 1 The Systems-engineering Process Trading Requirements We use the requirements loopa necessary and.
Advertisements

Satellite Communication
Understanding the Systems Engineering Process
1 Air Launch System Project Proposal February 11, 2008 Dan Poniatowski (Team Lead) Matt Campbell Dan Cipera Pierre Dumas Boris Kaganovich Jason LaDoucer.
MN Space Grant Community College Quadcopter Competition General advice about giving the team oral presentation at the competition, from Professor.
Protocol & Test Review Spaceport America Student Launch University/Institution Team Members Date.
Proposal Analysis Review NMSGC Student Launch University/Institution Team Members Date.
Data Test Review Spaceport America Student Launch University/Institution Team Members Date.
Flight Readiness Review New Mexico Space Grant Consortium University/Institution Team Members Date.
By Matthew Patterson. L ow E arth O rbit N anosatellite I ntegrated D istributed A lert S ystem.
14/06/20151 MORE Requirements seen from ESA Pedro Pablos 1 st MORE Team Meeting 27 Febrero 2007.
Paul “Trey” Karsten Marcell Smalley Shunsuke Miyazaki Brynn Larson Terek Campbell Marcus Flores 11/25/09 Final Revision.
1 Spacecraft Thermal Design Introduction to Space Systems and Spacecraft Design Space Systems Design.
Spacecraft Design and Sizing Dr Andrew Ketsdever MAE 5595 Lesson 14.
Project Management 30 January. Odds and ends Tournament on the webweb In the newsnews.
Your Presentation Title Names of Team members Advisor name EE496A Midterm Presentation Fall, 2006.
UHM CanSat Team Members: Chris Ho: Team master, software Tyson Fukuyama: Hardware.
AAE450 Senior Spacecraft Design Dorrie Byford Week 1: January 18 th, 2007 Communications Group Leader / Autonomous Rendezvous Team Member / Website Designer.
Satellite communications and the environment of space Images: NASA.
Space Engineering Institute (SEI) Space Based Solar Power Space Engineering Research Center Texas Engineering Experiment Station, Texas A&M University.
CSULB EE400D Documentation Instructional Series
Mae Jemison Space Scientist
Planning. SDLC Planning Analysis Design Implementation.
1 Formation Flying Rachel Winters Matt Whitten Kyle Tholen Matt Mueller Shelby Sullivan Eric Weber Shunsuke Hirayama Tsutomu Hasegawa Aziatun Burhan Masao.
1 Electrical Power System By Aziatun Burhan. 2 Overview Design goal requirements throughout mission operation: Energy source generates enough electrical.
Critical Design Review Team Name University/Institution Team Members Date.
Author Name Page 1 CNES’07 Peer Review 4/17/02 CNES’07 Mars Premier Peer Review Rendezvous and Sample Capture OS Beacon Electronics And Power System Mark.
Miscellaneous Notes: This is a bare-bones template – make it fancier if you wish, but be sure to address at least the items listed here. Basically this.
The Pursuit for Efficient S/C Design The Stanford Small Sat Challenge: –Learn system engineering processes –Design, build, test, and fly a CubeSat project.
1 Project Name Solar Sail Project Proposal February 7, 2007 Megan Williams (Team Lead) Eric Blake Jon Braam Raymond Haremza Michael Hiti Kory Jenkins Daniel.
Workshops Tech Com: Progress Reports Terminology from the first class period Goal: What it is you are trying to accomplish; the bottom line. Milestone:
1 Formation Flying Shunsuke Hirayama Tsutomu Hasegawa Aziatun Burhan Masao Shimada Tomo Sugano Rachel Winters Matt Whitten Kyle Tholen Matt Mueller Shelby.
ReVeal Passive Illumination by Radar (PAIR). Overview Payload / Mission Communication Launch Orbit Power Thermal Attitude Propulsion Finance.
Tielong Zhang On behalf of the CGS Team in the Institute of Geology and Geophysics, Chinese Academy of Science Spacecraft System and Payload China Geomagnetism.
1. 2 Purpose of This Presentation ◆ To explain how spacecraft can be virtualized by using a standard modeling method; ◆ To introduce the basic concept.
Different Coverage Patterns for a Single Satellite and Constellation of Satellites in Real Time with the STK Pedro A. Capó-Lugo Graduate Student Dr. Peter.
Space unit Life in Space.
Preliminary Design of NEA Detection Array Contractor 2 Kim Ellsworth Brigid Flood Nick Gawloski James Kim Lisa Malone Clay Matcek Brian Musslewhite Randall.
By: Christiano Daniel Abadi. Deliverables/Achievements in Spring 2000: 8 Systems Engineering Documents Overall and power budgets Gantt Chart for Preliminary.
DINO PDR 23 October 2015 DINO Systems Team Jeff Parker Anthony Lowrey.
Pre-Project Components
And Redundancy -By Brandon Fuller & Christopher Gossett.
SOW / Open Workbench By Wilmer Arellano Summer 2013.
Chapter 13 Section 3 – pg 515 Exploring Space Today.
1 Jet Propulsion Laboratory JPL Flight Team Adam Nikolic Josh Ruggiero Bob Hoffman Dusty Terrill.
1 Weekly Summary Weekly Summary Formation Flight AEM4332 Spring Semester March 7,2007 Masao SHIMADA.
The final Space Shuttle has landed… Now what??. The Space Shuttle Since 1981, NASA space shuttles have been rocketing from the Florida coast into Earth.
GE 121 – Engineering Design Engineering Design GE121 Managing The Design Process Part II Lecture 11B.
Wes Ousley June 28, 2001 SuperNova/ Acceleration Probe (SNAP) Thermal.
Amy Blas Hawaii Space Flight Laboratory University of Hawaii.
S.H.I.E.L.D. CRITICAL DESIGN REVIEW Addison, Travis, Jared, Evan, Aaron, Matt 10/14/08.
Presented by G. Hena Mercy Sugirthem G. Hena Mercy Sugirthem M. Sharmila M. Sharmila.
Micro Arcsecond X-ray Imaging Mission Pathfinder (MAXIM-PF) Mechanical George Roach Dave Peters 17 May 2002 “Technological progress is like an axe in the.
 From SmallSat to CubeSat: Reducing Mass Size and Cost Jeremy Straub 1, Ronald Fevig 2, Todd Borzych 2, Chris Church 2, Curt Holmer 2, Martin Hynes 2,
Wayfarer Ryan Stelzer Dr. David Gaylor April 16 th, 2016 Arizona Space Grant Symposium.
What is a WBS? A Work Breakdown Structure is not a list of tasks, a schedule or an organization chart. Rather it provides the basis on which a task.
Eric Weber (1/14)1 Configuration and Structural Design Eric Weber Tasks –Preliminary hardware research –Preliminary transmission research –Materials Research.
Session VIII: Work Plan and Budget Plan
Simulation-to-Flight 1 Additional Resources:
By Wilmer Arellano Spring 2010
Planetary Lander PDR Team Name
Monitoring Implementation and Sustainability
Maxim Pathfinder Prework 16 August 1999
Chapter 16 Section 8 What is the space shuttle?
Team member, Team member and Team member
Team Super 8: Sat Morpheus Final Presentation
Classroom Rocket Scientist
Team member, Team member and Team member
Types of Spacecraft The FRAME Routine Key Topic is about…
<Your Team # > Your Team Name Here
Presentation transcript:

1 Formation Flying Project Proposal 2/5/07 Rachel Winters (Team Lead) Aziatun Burhan Tsutomu Hasegawa Shunsuke Hirayama Matt Mueller Masao Shimada Shelby Sullivan Kyle Tholen Eric Weber Matt Whitten

2 Objective The objective of this project is to fly one or more satellites in formation around a space shuttle. The satellites will carry cameras to detect damage on the outside of the shuttle.

3 Requirements Design must meet University Nanosat Requirements –Mass < 50 kg –Volume < 60x60x50 cm cube Satellites provide visible coverage of complete exterior of shuttle Duration of visible inspection should last at least 24 hours –Satellites must have power source capable of keeping cameras and other systems operational for at least 24 hours.

4 Expectations Explain the results of all trade studies Demonstrate that the design meets the requirements of the University Nanosat program. Demonstrate that the power supply is sufficient for the mission Demonstrate that the spacecraft and its components will stay within allowable temperature ranges Demonstrate that the spacecraft can perform this mission.

5 Major Tasks 1. Identify COTS cameras, transmitters, and other essential hardware for the design 2. Design relative orbit geometries that provide full visible coverage 3. Determine and quantify the major disturbances affecting relative orbital motion 4. Determine the mass, size and power requirements for the camera(s) and transmitter 5. Determine all required systems 6. Perform trade study between solar cells + battery vs. battery only designs 7. Perform trade study between single vs. multiple cameras 8. Perform a trade study between expendable and recoverable designs 9. Perform a trade study between a single spacecraft vs. multiple spacecraft 10. Design a configuration that meets all requirements

6 Team Organization

7 Task Breakdown 1. Identify COTS cameras, transmitters, and other essential hardware for the design –Research essential satellite hardware (ie - transmitters, antennas, propulsion system) –Research mission specific hardware (ie - COTS camera, localized positioning system) 2. Design relative orbit geometries that provide full visible coverage 1.Determine orbit of ISS to use as reference 2.Become familiar with STK software to model orbits 3.Research relative orbits 4.Determine actual orbit of satellites

8 Task Breakdown (Continued...) 3. Determine and quantify the major disturbances affecting relative orbital motion –Assume location in orbit –Research causes of disturbances –Effects of geo-potential orbits –Previous work on counteracting disturbances –Design method to counteract disturbances 4. Determine the mass, size and power requirements for the camera(s) and transmitter –Determine specs for each component Volume Mass Power Consumption –Determine total satellite configuration

9 5. Design satellite configuration –Components positioning –Case and Structure –Solid model –Animation with Space shuttle 6. Determine all required systems –Thermal Control subsystem Determine input parameters Determine thermal environments Thermal mathematical model Thermal controls element Arrangement of satellite components –Communications subsytem Transmission rate Transmission method Communication circuit design Constitution, mass, power consumption Task Breakdown (Continued...)

10 6. Perform trade study between solar cells + battery vs. battery only designs –Research Solar cells & batteries –List pros and cons –Model both cases 7. Perform trade study between single vs. multiple cameras –Find related topics –Summarize information –List pros and cons –Model both cases Task Breakdown (Continued...)

11 8. Perform a trade study between expendable and recoverable designs –Find related topics –Summarize information –List pros and cons –Model both cases 9. Perform a trade study between a single spacecraft vs. multiple spacecraft –Find related topics Estimate equipment cost Recovery/repair Method of recovery –Summarize information –List pros and cons –Model both cases Task Breakdown (Continued...)

Design a configuration that meets all requirements –Solid model of space shuttle –Determine specific requirements that need to be completed –Testing to see that requirements are met Task Breakdown (Continued...)

13 Gantt Chart

14 Questions Volume nanosat requirement, are we allowed to increase volume after launch? (ie- extend antenna) Do we transmit the signal to the shuttle or back to earth? Do we have preprogrammed flight plan or does it change according to signals from transmitter? How are we reaching low earth orbit? (On the space shuttle or via external rocket) Do we need to determine how to get satellite into orbits? Do we need to provide visible coverage of the shuttle only once, say if we were checking for damage during takeoff, or is our goal to provide coverage for the entire duration of the shuttle mission?

15 First major task –Name of sub-task A (Last name of assigned person) Description –Name of sub-task B (Last name of assigned person) Description – Second major task –Name of sub-task A (Last name of assigned person) Description – and so on… –The sub-tasks need to be very specific –You may have SEVERAL sub-tasks under each major task. That’s great. –Ideally, each sub-task can be conducted by a single person. –If multiple people are required to complete a sub-task, you need to clearly define the roles of everyone involved Use more slides as necessary to complete the breakdown

16 Schedule Your Gantt chart should go here Use a PM software program of your choice to make the Gantt chart Include an image of it here It will likely need to be shrunk considerably to fit on a single page If the text of the full schedule is too small to read, break it up into smaller parts so that it is legible When making your schedule, consider the following: –Be aware of dependent tasks. These are tasks can only begin after other tasks have been completed. –Be aware of the workload for each team member. Are there periods of time when certain members are idle? Times when they are worked too heavily? –If you feel that there is not enough time to do all of the work you are proposing to do, maybe you need to scale back the goals/expectations of the project. If this is the case, come up with a suggestion and we can decide what to do. –Use additional slides if necessary, rather than cramming it all in too closely.