CTV: Damocles. Method of Configuration Restrictions on Component Placement Mission Accomplishments Final Configuration and Specifications
|
|
- Oswin Boone
- 5 years ago
- Views:
Transcription
1 CTV: Damocles Method of Configuration Restrictions on Component Placement Mission Accomplishments Final Configuration and Specifications
2 7 Wonders of Damocles Manned Interplanetary Travel Artificial Gravity Refueling on an Asteroid Internet, Video, and Cerial Positioning System Carrying Science Material Return To Earth Reusable for Future Missions
3 Designing Damocles All recoverable components must be shielded by a single piece shield 8.8 m Aeroshell
4 Designing Damocles Attic -Crew Cabin contains center of mass during aerocapture. -MORS Engine and Capsule Storage located on opposite end. Crew Living Area Aeroshell
5 Designing Damocles -Reactor on opposite end to allow heat rejection. Capsule MORS -Optical communication unobstructed by primary tanks. PWR Reactor Telescope Attic Crew Living Area Aeroshell
6 Designing Damocles Capsule MORS Reactor Chassis MPDs Telescope Gravity Cables Attic Aeroshell -Structure built to house components and reel system for tethers. -MPD thrusters placed on tethers. Crew Living Area
7 Designing Damocles -Central structure assembled and launched as single piece -Propellant tanks attach around chassis LH 2 LOX Kick Motor Ceres Regime Motor
8 Designing Damocles - Tanks fit around central structure Primary Tanks Secondary Tanks Chassis Structure
9 Designing Damocles -Capsule is able to dock below secondary tanks Secondaries Capsule Primary Tanks Chassis Structure
10 CTV Propulsion Kick Engines (LH 2 /LOX) kg, 1500 kn of sec Isp (each) 3 Engines on Primaries 3 Engines on Secondaries Ceres Regime Engines (LH 2 /LOX) kn of sec Isp 3 Engines, throttleable to 50% Hill, Michael Propulsion
11 CTV Propulsion Electric Propulsion System (GH 2 ) 51.5 kg, 10 N of 5000 sec Isp (Each) Requires 490 kw/thruster Use 4 thrusters Spin-up/Attitude Thrusters (MMH/N 2 O 4 ) 0.93 kg, 50 N of 328 sec Isp 6 Total on vehicle Hill, Michael Propulsion
12 Nuclear Reactor Update Power (kwe) Total Mass (kg) PMAD Heat Reject Power Conv. HSHX Shield (LiH/W) Reactor Specific Power (kg/kwe) Width (m) 2.0 Height (m) 1.6 Volume (m3) ~6.0 Radiator Area (m2) 3220 Crenwelge, Drew By Drew Crenwelge Power Group
13 Communication System CTV Power (kw) Mass (kg) Volume (m 3 ) ) Optical TDRS Receiving Dish TDRS Transmitting Dish Transponder Phased Array Total Optical Telescope Specifications Diam Rec/Trans (m) Length Rec /Trans(m) 2/ /0.5 Communication totals for all operations Optical Telescope Specifications now final Phased Array communicates with Capsule TDRS Dish system communicates with satellites in GEO which relay the signal to Earth Justin Axsom Communication
14 The Kwan Stretch Courtesy of Alexander Roth
15 The Kwan Stretch Courtesy of Alexander Roth
16 Capsule Storage & MORS Courtesy of Alexander Roth
17 Compact Configuration Courtesy of Alexander Roth
18 Configuration of Damocles Courtesy of Alexander Roth
19 Vehicle Specifications Crew Cabin Storage Attic Capsule IonRail Chassis Crew Side Propellant Main Propellant 38,373 kg kg 9834 kg 306 kg kg 1300 kg kg
20 Vehicle Specifications Damocles V-14.1 Pontiac G6 GT mpg 1, mph sec 15.5 sec hp 48,486, Top Speed 15,658 mph 120 mph Range 479,805,407 mi 320 mi ΔV 7 km/s km/s T/W Isp s s λ
PERSPECTIVES ON PROPULSION FOR FUTURE SPACE MISSIONS
PERSPECTIVES ON PROPULSION FOR FUTURE SPACE MISSIONS Keynote, NIAC Fellows Meeting March 24, 2004, Crystal City, VA By Jerry Grey First Task: Earth to Orbit (1) Existing Expendable Launch Vehicles: Atlas-V,
More informationIn Space Propulsion Overview January Outline. Les Johnson Manager, In Space Propulsion Technology Projects Office
In Space Propulsion Overview 14-17 January 2003 Outline Les Johnson Manager, In Space Propulsion Technology Projects Office In-Space Propulsion Program Overview Objective Develop in-space propulsion technologies
More informationNASA TA-02 In-space Propulsion Roadmap Priorities
NASA TA-02 In-space Propulsion Roadmap Priorities Russell Joyner Technical Fellow Pratt Whitney Rocketdyne March 22, 2011 TA02 In-space Propulsion Roadmap High Thrust (>1kN or >224-lbf) Focus The Overarching
More informationDemocritos a Europe funded project preparing demonstrators for high power nuclear electric space propulsion
Democritos a Europe funded project preparing demonstrators for high power nuclear electric space propulsion Mr. Frédéric Masson, Mr. Jean-Marc Ruault 1 Dr. Jean-Claude Worms, Dr. Emmanouil Detsis 2 Mr.
More informationPanel Session IV - Future Space Exploration
The Space Congress Proceedings 2003 (40th) Linking the Past to the Future - A Celebration of Space May 1st, 8:30 AM - 11:00 AM Panel Session IV - Future Space Exploration Canaveral Council of Technical
More informationScience Plenary II: Science Missions Enabled by Nuclear Power and Propulsion. Chair / Organizer: Steven D. Howe Center for Space Nuclear Research
Science Plenary II: Science Missions Enabled by Nuclear Power and Propulsion Chair / Organizer: Steven D. Howe Center for Space Nuclear Research Distinguished Panel Space Nuclear Power and Propulsion:
More informationTEMPO Apr-09 TEMPO 3 The Mars Society
TEMPO 3 1 2 TEMPO 3 First step to the Fourth Planet Overview Humans to Mars Humans in Space Artificial Gravity Tethers TEMPO 3 3 Humans to Mars How? Not one huge ship W. von Braun Send return craft first
More informationCOMPARATIVE ASSESSMENT OF HUMAN-MARS-MISSION TECHNOLOGIES AND ARCHITECTURES
COMPARATIVE ASSESSMENT OF HUMAN-MARS-MISSION TECHNOLOGIES AND ARCHITECTURES D.F. LANDAU and J.M. LONGUSKI School of Aeronautics and Astronautics, Purdue University, West Lafayette, IN, 47907-2023, USA
More informationElectric Solar Wind Sail tether payloads onboard CubeSats
Electric Solar Wind Sail tether payloads onboard CubeSats Jouni Envall, Petri Toivanen, Pekka Janhunen Finnish Meteorological Institute, Helsinki, Finland (jouni.envall@fmi.fi) Outline E-sail & Coulomb
More informationlaunch probability of success
Using Architecture Models to Understand Policy Impacts Utility 1 0.995 0.99 Policy increases cost B C D 10 of B-TOS architectures have cost increase under restrictive launch policy for a minimum cost decision
More informationWHAT IS A CUBESAT? DragonSat-1 (1U CubeSat)
1 WHAT IS A CUBESAT? Miniaturized satellites classified according to height (10-30 cm) Purpose is to perform small spacecraft experiments. Use has increased due to relatively low cost DragonSat-1 (1U CubeSat)
More informationSolar Power Satellite, Space Elevator, and Reusable Launch
AIAA-2010-791690 Solar Power Satellite, Space Elevator, and Reusable Launch Dr. James A. Martin Consultant, Associate Editor JSR Space 2010 Conference Anaheim, CA August 30, 2010 Solar Power Satellites
More informationRed Dragon. Feasibility of a Dragon-derived Mars lander for scientific and human-precursor missions. May 7, 2013
Red Dragon Feasibility of a Dragon-derived Mars lander for scientific and human-precursor missions May 7, 2013 John S. Karcz (john.s.karcz@nasa.gov) NASA Ames Research Center 1 Overview We are studying
More informationNear Term Space Settlement: Risk Reduction Missions
Near Term Space Settlement: Risk Reduction Missions Kent Nebergall Macroinvent.com Mars Society Conference, 2017 2017 Kent Nebergall All rights reserved. The Grand Challenges of Space Settlement (2014)
More informationHYDROS Development of a CubeSat Water Electrolysis Propulsion System
HYDROS Development of a CubeSat Water Electrolysis Propulsion System Vince Ethier, Lenny Paritsky, Todd Moser, Jeffrey Slostad, Robert Hoyt Tethers Unlimited, Inc 11711 N. Creek Pkwy S., Suite D113, Bothell,
More informationUnderstand that technology has different levels of maturity and that lower maturity levels come with higher risks.
Technology 1 Agenda Understand that technology has different levels of maturity and that lower maturity levels come with higher risks. Introduce the Technology Readiness Level (TRL) scale used to assess
More informationPicture of Team. Bryce Walker. Charles Swenson. Alex Christensen. Jackson Pontsler. Erik Stromberg. Cody Palmer. Benjamin Maxfield.
RUNNER Alex Christensen, William Hatch, Keyvan Johnson, Jorden Luke, Benjamin Maxfield, Andrew Mugleston, Cody Palmer, Jackson Pontsler, Jacob Singleton, Nathan Spencer, Erik Stromberg, Bryce Walker, Cameron
More informationCYLICAL VISITS TO MARS VIA ASTRONAUT HOTELS
CYLICAL VISITS TO MARS VIA ASTRONAUT HOTELS Presentation to the NASA Institute of Advanced Concepts (NIAC) 2000 Annual Meeting by Kerry T. Nock Global June 7, 2000 Global TOPICS MOTIVATION OVERVIEW SIGNIFICANCE
More informationCredits. National Aeronautics and Space Administration. United Space Alliance, LLC. John Frassanito and Associates Strategic Visualization
A New Age in Space The Vision for Space Exploration Credits National Aeronautics and Space Administration United Space Alliance, LLC John Frassanito and Associates Strategic Visualization Coalition for
More informationCYCLIC VISITS TO MARS VIA ASTRONAUT HOTELS
CYCLIC VISITS TO MARS VIA ASTRONAUT HOTELS OR THE INTERPLANETARY RAPID TRANSIT (IRT) SYSTEM Presentation to the NASA Institute for Advanced Concepts (NIAC) 4th Annual Meeting Lunar and Planetary Institute,
More informationHuman Exploration of Mars Design Reference Architecture 5.0
Human Exploration of Mars Design Reference Architecture 5.0 https://ntrs.nasa.gov/search.jsp?r=20090012109 2018-07-20T17:22:56+00:00Z National Aeronautics and Space Administration Bret G. Drake Lyndon
More informationUranus Exploration Challenges
Uranus Exploration Challenges Steve Matousek Workshop on the Study of Icy Giant Planet (2014) July 30, 2014 (c) 2014 California Institute of Technology. Government sponsorship acknowledged. JPL URS clearance
More informationDream Chaser for European Utilization (DC 4 EU):
54th European Space Science Committee Plenary Meeting 22-24 November 2017 German Aerospace Centre DLR Obepfaffenhofen, Germany Presenter: Dr. Marco Berg Dream Chaser for European Utilization (DC 4 EU):
More informationMission to Earth Moon Lagrange Point by a 6U CubeSat: EQUULEUS
Mission to Earth Moon Lagrange Point by a 6U CubeSat: EQUULEUS (EQUilibriUm Lunar-Earth point 6U Spacecraft) Ryu Funase Associate Professor, EQUULEUS project manager, Univ. of Tokyo EQUULEUS Project Team
More informationA CubeSat-Based Optical Communication Network for Low Earth Orbit
A CubeSat-Based Optical Communication Network for Low Earth Orbit Richard Welle, Alexander Utter, Todd Rose, Jerry Fuller, Kristin Gates, Benjamin Oakes, and Siegfried Janson The Aerospace Corporation
More informationYour final semester project papers are due in ONE WEEK, Thu April 28th (last day of class). Please return your marked-up First draft.
The Home Stretch Your final semester project papers are due in ONE WEEK, Thu April 28th (last day of class). Please return your marked-up First draft. Final Exam: 12:30pm, Friday May 6th, 2hrs. Any homework/drafts/etc.
More informationCubeSat Standard Updates
CubeSat Standard Updates Justin Carnahan California Polytechnic State University April 25, 2013 CubeSat Developers Workshop Agenda The CubeSat Standard CDS Rev. 12 to Rev. 13 Changes The 6U CubeSat Design
More informationChapter 2 Planning Space Campaigns and Missions
Chapter 2 Planning Space Campaigns and Missions Abstract In the early stages of designing a mission to Mars, an important measure of the mission cost is the initial mass in LEO (IMLEO). A significant portion
More informationAVSS Project. ENAE483 Fall 2012
AVSS Project ENAE483 Fall 2012 Team D9: Jason Burr Vera Klimchenko Grant McLaughlin Johnathan Pino Link Budget Analysis Maximum Earth-Moon Transmission Distance R M D R M R e Moon 406,700 km Earth Ku Band
More informationAction Vehicle Action Surface Systems. -Exc. -Processing -Growth
Action Vehicle Action Surface Systems FIT -LEO Cycler UH -Habs FIT -Lunar Cycler -Rovers FIT -Mars cycler -Cabs FIT -CAB -Power -Lander/Small/Larg e -ETO UH -Exc. -Processing -Growth Buzz: The purpose
More informationAbstract- Light Kite. things, finding resources and using them for our own use.
Abstract- Light Kite Using solar sail and laser propulsion as alternative fuel for deep space travel can greatly increase our knowledge of the outside universe. Solar sails attached to the spacecraft captures
More informationHuman mission to Mars: The concept
Technical report n 2012-5-242 Human mission to Mars: The 2-4-2 concept Jean Marc Salotti Laboratoire de l Intégration du Matériau au Système (UMR5218) Ecole Nationale Supérieure de Cognitique Institut
More information; ; IR
MS-2-2.5 SATELLITE The MS-2-2.5 satellite is designed for Earth Remote Sensing with the use of high resolution IR and multi-band imager. The satellite performs natural and man-caused disasters monitoring,
More informationAsteroid Redirect Mission and Human Exploration. William H. Gerstenmaier NASA Associate Administrator for Human Exploration and Operations
Asteroid Redirect Mission and Human Exploration William H. Gerstenmaier NASA Associate Administrator for Human Exploration and Operations Leveraging Capabilities for an Asteroid Mission NASA is aligning
More informationEnabling Technologies for robotic and human Exploration
Enabling Technologies for robotic and human Exploration Norbert Frischauf,, Bruno Gardini, Alain Pradier,, Dietrich Vennemann Aurora Programme Office IAA/ESA Workshop ESA/ESTEC, 22-23/09/2003 22-23/09/2003-1-
More informationIntroduction to MATE-CON. Presented By Hugh McManus Metis Design 3/27/03
Introduction to MATE-CON Presented By Hugh McManus Metis Design 3/27/03 A method for the front end MATE Architecture Tradespace Exploration A process for understanding complex solutions to complex problems
More informationCreating the Cislunar Economy
Copyright 2018 George Sowers All Rights Reserved Creating the Cislunar Economy George Sowers February 26, 2018 2 Photo & video courtesy United Launch Alliance Revolution Timeframe Location Energy capture
More informationSpace Tethers Technology Status and The Way Forward
Space Tethers Technology Status and The Way Forward Rob Hoyt Tethers Unlimited, Inc 11711 N. Creek Pkwy S., Suite D113 Bothell, WA 98011 425-486- 0100 hoyt@tethers.com www.tethers.com 1 DefiniPons Space
More informationReducing the Challenges Posed by Titan Missions
Reducing the Challenges Posed by Titan Missions Presentation to the Satellites Panel of the Planetary Science Decadal Survey Kim Reh, John Elliott, Jeffrey Hall Deputy Manager, Solar System Mission Formulation
More informationProximity Operations Nano-Satellite Flight Demonstration (PONSFD) Overview
Proximity Operations Nano-Satellite Flight Demonstration (PONSFD) Overview April 25 th, 2013 Scott MacGillivray, President Tyvak Nano-Satellite Systems LLC 15265 Alton Parkway, Suite 200 Irvine, CA 92618-2606
More informationSSL Payload Orbital Delivery System (PODS) FedEx to GTO/GEO
SSL Payload Orbital Delivery System (PODS) FedEx to GTO/GEO June 10th, 2015 For more information, contact: Al Tadros, SSL Email: al.tadros@sslmda.com Tel: (650) 714-0439 Laurie Chappell, SSL Email: laurie.chappell@sslmda.com
More informationDay 1 Part1 course. Basics of satellite communications
Day 1 Part1 course Basics of satellite communications 1 Historical Perspective of satellite communications 2 1- Birth of satellite communications Satellites are able to fulfill a number of roles. One of
More informationAustere Human Missions to Mars
Austere Human Missions to Mars Hoppy Price Jet Propulsion Laboratory, California Institute of Technology Alisa Hawkins, Torrey Radcliffe The Aerospace Corporation AIAA Space 2009 Conference Pasadena, California
More informationFor Winter /12/2006
AE483 Organizational Meeting For Winter 2007 12/12/2006 Today s Meeting Basic info about the course Course organization Course output (deliverables) Proposed projects Ballot for project selection due in
More informationThe SunCube FemtoSat Platform: A Pathway to Low-Cost Interplanetary Exploration
The SunCube FemtoSat Platform: A Pathway to Low-Cost Interplanetary Exploration Jekan Thanga, Mercedes Herreras-Martinez, Andrew Warren, Aman Chandra Space and Terrestrial Robotic Exploration (SpaceTREx)
More informationCubeSat Solid Rocket Motor Propulsion Systems providing DVs greater than 500 m/s
CubeSat Solid Rocket Motor Propulsion Systems providing DVs greater than 500 m/s Kevin L. Zondervan, Jerry Fuller, Darren Rowen, Brian Hardy, Chris Kobel, Shin-Hsing Chen, Phillip Morrison, Timothy Smith,
More informationFORMATION FLYING PICOSAT SWARMS FOR FORMING EXTREMELY LARGE APERTURES
FORMATION FLYING PICOSAT SWARMS FOR FORMING EXTREMELY LARGE APERTURES Presented at the ESA/ESTEC Workshop on Innovative System Concepts February 21, 2006 Ivan Bekey President, Bekey Designs, Inc. 4624
More informationSpace Technology Mission Directorate
National Aeronautics and Space Administration Space Technology Mission Directorate Maryland Space Business Roundtable Presented by: Stephen Jurczyk Associate Administrator, STMD October 17, 2017 www.nasa.gov/spacetech
More informationECE 6390: Satellite Communications and Navigation Systems TEST 1 (Fall 2010)
Name: GTID: ECE 6390: Satellite Communications and Navigation Systems TEST 1 (Fall 2010) Please read all instructions before continuing with the test. This is a closed notes, closed book, closed friend,
More informationInnovation Needs Support: Two Examples of German Support Strategy in Satcom
The Space Congress Proceedings 2016 (44th) The Journey: Further Exploration for Universal Opportunities May 25th, 10:45 AM Innovation Needs Support: Two Examples of German Support Strategy in Satcom Frank
More informationWHAT WILL AMERICA DO IN SPACE NOW?
WHAT WILL AMERICA DO IN SPACE NOW? William Ketchum AIAA Associate Fellow 28 March 2013 With the Space Shuttles now retired America has no way to send our Astronauts into space. To get our Astronauts to
More informationAustere Human Missions to Mars
Austere Human Missions to Mars Hoppy Price 1 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109 Alisa M. Hawkins 2, Torrey O. Radcliffe 3 The Aerospace Corporation, El Segundo,
More informationSolar Observing Low-frequency Array for Radio Astronomy (SOLARA)
Solar Observing Low-frequency Array for Radio Astronomy (SOLARA) Exploring the last frontier of the EM spectrum Mary Knapp, Dr. Alessandra Babuscia, Rebecca Jensen-Clem, Francois Martel, Prof. Sara Seager
More informationLesson Title: Using Waves to Communicate Subject Grade Level Timeline. Physical Science minutes. Objectives
Lesson Title: Using Waves to Communicate Subject Grade Level Timeline Physical Science 7-8 45 minutes Objectives This lesson investigates the difference between longitudinal waves and transverse waves,
More informationInterplanetary CubeSats mission for space weather evaluations and technology demonstration
Interplanetary CubeSats mission for space weather evaluations and technology demonstration M.A. Viscio, N. Viola, S. Corpino Politecnico di Torino, Italy C. Circi*, F. Fumenti** *University La Sapienza,
More informationECE 6390: Satellite Communications and Navigation Systems TEST 1 (Fall 2004)
Name: GTID: ECE 6390: Satellite Communications and Navigation Systems TEST 1 (Fall 2004) Please read all instructions before continuing with the test. This is a closed notes, closed book, closed friend,
More informationSSL Payload Orbital Delivery System (PODS) FedEx to GTO/GEO
SSL Payload Orbital Delivery System (PODS) FedEx to GTO/GEO For more information, contact: May 27 th, 2015 Al Tadros, SSL Email: al.tadros@sslmda.com Tel: 1-650-714-0439 OR Dan King, MDA Email: dan.king@mdacorporation.com
More informationCharacteristics of Apex Anchors
Characteristics of Apex Anchors Peter A. Swan, Ph.D. President, Member BofD s International Space Elevator Consortium Member IAA, Fellow, TBIS, AIAA International Space Elevator Conference Seattle s Museum
More informationQuestions for the 2018 RASC-AL Q&A Session
2018 RASC-AL Q&A Transcript Monday, October 23, 2017 Note from Patrick Troutman, LaRC Human Exploration Strategic Analysis Lead: RASC-AL is the Human Exploration Program s way of reaching out to the university
More informationCubesats and the challenges of Docking
Cubesats and the challenges of Docking Luca Simonini Singapore Space Challenge 2017 Education outreaches, Thales Solutions Asia Pte. Ltd. August the 30 th 2017 September the 6 th 2017 www.thalesgroup.com
More informationEnabling The Future: NASA s Routes to Future Large UV/Optical Telescopes in Space
Enabling The Future: NASA s Routes to Future Large UV/Optical Telescopes in Space April 10, 2003 Space Telescope Science Institute Harley Thronson Director of Technology Office of Space Science National
More informationNWO Servicing NGST. Chuck Lillie November 6, 2008
NWO Servicing NGST Chuck Lillie November 6, 2008 Design for Servicing Future space observatories should be designed to enable on-orbit servicing to: Replenish expendables Replace limited-lifetime items
More informationIAC-18.A5.1.4x Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway
IAC-18.A5.1.4x46653 Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway Timothy Cichan a*, Stephen A. Bailey b, Adam Burch c, Nickolas W. Kirby d a Space Exploration Architect,
More informationPAYLOAD DESIGN FOR A MICROSATELLITE II. Aukai Kent Department of Mechanical Engineering University of Hawai i at Mānoa Honolulu, HI ABSTRACT
PAYLOAD DESIGN FOR A MICROSATELLITE II Aukai Kent Department of Mechanical Engineering University of Hawai i at Mānoa Honolulu, HI 96822 ABSTRACT Conventional satellites are extremely large, highly expensive,
More informationINTRODUCTION The validity of dissertation Object of investigation Subject of investigation The purpose: of the tasks The novelty:
INTRODUCTION The validity of dissertation. According to the federal target program "Maintenance, development and use of the GLONASS system for 2012-2020 years the following challenges were determined:
More informationCubeSat Navigation System and Software Design. Submitted for CIS-4722 Senior Project II Vermont Technical College Al Corkery
CubeSat Navigation System and Software Design Submitted for CIS-4722 Senior Project II Vermont Technical College Al Corkery Project Objectives Research the technical aspects of integrating the CubeSat
More informationLunar Exploration Communications Relay Microsatellite
Lunar Exploration Communications Relay Microsatellite Paul Kolodziejski Andrews Space, Inc. 505 5 th Ave South, Suite 300 Seattle WA 98104 719-282-1978 pkolodziejski@andrews-space.com Steve Knowles Andrews
More informationScience and Technology SATellite Program of KOREA
Science and Technology SATellite Program of KOREA November 2, 2004-1- Contents Introduction KITSAT (Korea Institute of Technology SATellite) STSAT (Science and Technology SATellite) KOMPSAT (KOrea( Multi-Purpose
More informationWireless Power Transmission Options
Wireless Power Transmission Options for Space Solar Power Seth Potter (1), Mark Henley (1), Dean Davis (1), Andrew Born (1), Joe Howell (2), and John Mankins (3) (1) The Boeing Company, (2) NASA Marshall
More informationSimulation of GPS-based Launch Vehicle Trajectory Estimation using UNSW Kea GPS Receiver
Simulation of GPS-based Launch Vehicle Trajectory Estimation using UNSW Kea GPS Receiver Sanat Biswas Australian Centre for Space Engineering Research, UNSW Australia, s.biswas@unsw.edu.au Li Qiao School
More informationSatellite Servicing and The Spirit of Innovation
Satellite Servicing and The Spirit of Innovation Presented to Goddard Contractors Association June 29, 2012 Frank Cepollina, Associate Director Satellite Servicing Capabilities Office Frank.J.Cepollina@nasa.gov
More informationCubeSat Communications Review and Concepts. Workshop, July 2, 2009
CubeSat Communications Review and Concepts CEDAR CubeSats Constellations and Communications Workshop, July 2, 29 Charles Swenson Presentation Outline Introduction slides for reference Link Budgets Data
More informationEnergy. on this world and elsewhere. Instructor: Gordon D. Cates Office: Physics 106a, Phone: (434)
Energy on this world and elsewhere Instructor: Gordon D. Cates Office: Physics 106a, Phone: (434) 924-4792 email: cates@virginia.edu Course web site available at www.phys.virginia.edu, click on classes
More informationTeam 6: University of Colorado Boulder (USA)
Global Trajectory Optimization Competition 7 Team 6: University of Colorado Boulder (USA) Team Lead: Jeff Parker parkerjs@colorado.edu Team: University of Colorado (USA) We are pleased to provide a solution
More informationSOME ASPECT AND PERSPECTIVES OF IMPLEMENTATION OF THE NATIONAL POLICY IN THE FIELD OF EXPLORATION AND PEACEFUL USES OF OUTER SPACE
SOME ASPECT AND PERSPECTIVES OF IMPLEMENTATION OF THE NATIONAL POLICY IN THE FIELD OF EXPLORATION AND PEACEFUL USES OF OUTER SPACE 1 Folie 1 NKS Raumfahrt, Dr. Adrian klein Background National Academy
More informationCubeSat Propulsion using Electrospray Thrusters
CubeSat Propulsion using Electrospray Thrusters Tom Roy, Nathaniel Demmons, Vlad Hruby, Nathan Rosenblad, Peter Rostler and Douglas Spence Busek Co., Natick, MA 01760 Paper SSC09-II-6 SmallSat Conference,
More informationIONOSFERE Satellite with APPT Based EPS
IONOSFERE Satellite with APPT Based EPS IEPC-2013-66 Presented at the 33rd International Electric Propulsion Conference, The George Washington University Washington, D.C. USA Nickolay N. Antropov 1 Research
More informationTechnologies for Outer Solar System Exploration
Technologies for Outer Solar System Exploration Ralph L. McNutt, Jr. Johns Hopkins University Applied Physics Laboratory and Member, OPAG Steering Committee 443-778-5435 Ralph.mcnutt@jhuapl.edu Space Exploration
More informationCommission for Moon, Mars and Beyond
Presentation of Summary Testimony of Jim Benson Founding Chairman, Chief Executive SpaceDev Commission for Moon, Mars and Beyond April 16, 2004 San Francisco Vision SpaceDev is a publicly traded space
More informationIAC-04-IAA THE SPACE ELEVATOR AND NASA S NEW SPACE INITIATIVE. Bradley C. Edwards Carbon Designs, Inc., United States
IAC-04-IAA.3.8.3.01 THE SPACE ELEVATOR AND NASA S NEW SPACE INITIATIVE Bradley C. Edwards Carbon Designs, Inc., United States brad_edwards@yahoo.com Ben Shelef Spaceward, United States ben@spaceward.com
More informationUWE-4: Integration State of the First Electrically Propelled 1U CubeSat
UWE-4: Integration State of the First Electrically Propelled 1U CubeSat Small Satellite Conference 2017 Philip Bangert A. Kramer, K. Schilling University Würzburg University Würzburg Experimental Satellites
More informationBuilding an L1 Depot in Phases: growing in step with operations on the Moon s surface. by Peter Kokh
Building an L1 Depot in Phases: growing in step with operations on the Moon s surface by Peter Kokh Building an L1 Depot in Phases: Strategic Location of the L1 Lagrange Area The Earth-Moon L1 point is
More informationCubeSat Launch and Deployment Accommodations
CubeSat Launch and Deployment Accommodations April 23, 2015 Marissa Stender, Chris Loghry, Chris Pearson, Joe Maly Moog Space Access and Integrated Systems jmaly@moog.com Getting Small Satellites into
More informationA Call for Boldness. President Kennedy September 1962
A Call for Boldness If I were to say, we shall send to the moon a giant rocket on an untried mission, to an unknown celestial body, and return it safely to earth, and do it right and do it first before
More informationSatellite Testing. Prepared by. A.Kaviyarasu Assistant Professor Department of Aerospace Engineering Madras Institute Of Technology Chromepet, Chennai
Satellite Testing Prepared by A.Kaviyarasu Assistant Professor Department of Aerospace Engineering Madras Institute Of Technology Chromepet, Chennai @copyright Solar Panel Deployment Test Spacecraft operating
More informationAvionics, Software, and Simulation ENAE483 Fall 2012
Avionics, Software, and Simulation ENAE483 Fall 2012 Team D7: Michael Cunningham Matthew Rich Michelle Sultzman Scott Wingate Presentation Overview Project Specifications Crew Capsule Design Choice Communications
More informationFuture Directions: Strategy for Human and Robotic Exploration. Gary L. Martin Space Architect
Future Directions: Strategy for Human and Robotic Exploration Gary L. Martin Space Architect September, 2003 Robust Exploration Strategy Traditional Approach: A Giant Leap (Apollo) Cold War competition
More informationTwo-way satellite Internet consists of:
1. INTRODUCTION Airborne Internet is a private, secure and reliable peer-to-peer aircraft communications network that uses the same technology as the commercial Internet. It is an implementation which
More informationSYSTEMS INTEGRATION AND STABILIZATION OF A CUBESAT
SYSTEMS INTEGRATION AND STABILIZATION OF A CUBESAT Tyson Kikugawa Department of Electrical Engineering University of Hawai i at Manoa Honolulu, HI 96822 ABSTRACT A CubeSat is a fully functioning satellite,
More informationEnergy. on this world and elsewhere. Instructor: Gordon D. Cates Office: Physics 106a, Phone: (434)
Energy on this world and elsewhere Instructor: Gordon D. Cates Office: Physics 106a, Phone: (434) 924-4792 email: cates@virginia.edu Course web site available at www.phys.virginia.edu, click on classes
More informationUNIT E: SPACE EXPLORATION
UNIT E: SPACE EXPLORATION S C I E N C E 9 1 Science 9 Unit E Section 2.0 TECHNOLOGICAL DEVELOPMENTS ARE MAKING SPACE EXPLORATION POSSIBLE AND OFFER BENEFITS ON EARTH. SECTI ON 2.0 Science 9 Unit E Section
More informationProject of space experiment "Shadow" on ISS
Project of space experiment "Shadow" on ISS New challenge and new opportunity for Amateur Radio Community 22.05.2004 1 Invitation Russian Aviation and Space Agency (Rosaviacosmos, the Russian analogue
More informationJHU/APL CubeSat Initiatives. Andy Lewin 19 April 2007
JHU/APL CubeSat Initiatives Andy Lewin 19 April 2007 Who is JHU/APL? Not-for-profit University research and development laboratory DoD chartered University Affiliated Research Center (UARC) Founded 1942
More informationCover. DLR-ESA Workshop on ARTES-11. SGEO: Implementation of of Artes-11. Dr. Andreas Winkler
Cover DLR-ESA Workshop on ARTES-11 SGEO: Implementation of of Artes-11 Dr. Andreas Winkler June June29, 29, 2006 2006 Tegernsee, Tegernsee, Germany Germany Slide 1 Table Table of of Contents - Introduction
More informationAstronomy 330. Final Papers. Presentation. Final
Astronomy 330 This class (Lecture 26): Space Travel David Zordan Sean Rohan Next Class: Visitations HW 11 is due! Note due on Tuesday! Final Papers You must turn final paper in with the graded rough draft.
More informationOn the Guidance and Control System of Epsilon Solid Rocket Launcher
On the Guidance and Control System of Epsilon Solid Rocket Launcher Y. Morita, M. Tamura, N. Ishii, T. Yamamoto Japan Aerospace Exploration Agency H. Ohtsuka, Y. Segawa and K. Tanaka IHI Aerospace Abstract
More informationIn this unit we are going to speak about satellite communications. Satellites are useful for connecting to remote areas, or when you want to
In this unit we are going to speak about satellite communications. Satellites are useful for connecting to remote areas, or when you want to broadcast video or data with minimal infrastructure. A communications
More informationTimepix in Deep Space Exploration Nuclear Electric Propulsion (NEP) to Near Earth Space Environment, EUROPA & MARS 1
Timepix in Deep Space Exploration Nuclear Electric Propulsion (NEP) to Near Earth Space Environment, EUROPA & MARS 1 Frank Jansen, Gerhard Grunwald, Tim Brandt et al., DLR Bremen, Oberpfaffenhofen, Braunschweig
More informationAnalysis of Potential for Venus-Bound Cubesat Scientific Investigations
Analysis of Potential for Venus-Bound Cubesat Scientific Investigations Image Sources: Earth Science and Remote Sensing Unit, NASA Johnson Space Center; JAXA / ISAS / DARTS / Damia Bouic / Elsevier inc.
More informationSSP Implementation: GEO vs. LEO. Reza Zekavat
SSP Implementation: GEO vs. LEO Reza Zekavat 1 GEO Orbit SBSP Cost? Maintenance? Environmental? Solar storm? 2 Installa1on and Launching Costs GEO: 35786 km (22300 Mile) Interna1onal Space Sta1on: 278
More information