DOCSLIB.ORG

Ares: Launch and Propulsion an Educator Guide with Activities in Science and Mathematics

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Ares: Launch and Propulsion an Educator Guide with Activities in Science and Mathematics National Aeronautics and Space Administration Ares: Launch and Propulsion An Educator Guide with Activities in Science and Mathematics Educational Product Educators Grades 5 – 12 EP-2009-02-32-MSFC Ares: Launch and Propulsion: An Educator’s Guide with Activities in Science and Mathematics Table of Contents Overview: Science Module . v Rocket Principles . viii Practical Rocketry . xii Teacher Guide: Pop Rocket Variables . 1 Student Activity: Pop Rocket Variables . 6 Student Text: Variables and Operational Definitions . 12 Teacher Guide: Pop Goes Newton . 15 Student Activity: Pop Goes Newton . 17 Student Text: Newton’s Laws of Motion and Rockets . 21 Teacher Guide: The History of Rocketry . 25 Teacher Guide: Launching Ares . 27 Student Text: From Earth to the Moon and Beyond . 34 Student Activity: Ground Challenge . 43 Student Activity: Moon Challenge . 47 Teacher Guide: Investigating Water Rockets: Abbreviated Approach . 51 Teacher Guide: Investigating Water Rockets: Comprehensive Approach . 55 Student Activity: Measuring Altitude . 62 Student Activity: What a Drag! . 65 Student Activity: Flying Straight . 68 Student Activity: Investigating Fin Shape or Size . 72 Student Activity: Investigating Fin Number and Placement . 78 Student Activity: Fly Like an Eagle . 81 Student Activity: Altitude vs. Water Volume . 84 Student Activity: Altitude vs. Water Pressure . 87 Student Activity: Weather or Not . 90 Teacher Guide: Fly Me High . 93 Student Activity: Fly Me High . 97 Teacher Guide: You Get What You Pay For . 103 Student Activity: You Get What You Pay For . 105 Appendix A: Example of a Completed Concept Definition Map . 108 Appendix B: Optional Activity . 109 Appendix C: Possible Options for the Ground Challenge . 110 Appendix D: Label Templates for Available Vehicles . 112 Appendix E: Templates for Representing Equipment and Supplies . 113 i Ares: Launch and Propulsion: An Educator’s Guide with Activities in Science and Mathematics Appendix F: Building a Bottle Rocket . 115 Appendix G: Water Bottle Rocket Launcher . 116 Appendix H: Transcripts . 119 Appendix I: NASA Altitude Tracker . 123 Appendix J: Safety Rules . 124 Appendix K: Safety Checklist . 126 Appendix L: Nose Cone Pattern . 127 Appendix M: Materials List . 128 Bibliography . 132 ii Ares: Launch and Propulsion: An Educator’s Guide with Activities in Science and Mathematics *This Educator Guide uses Traditional U.S. units of measure as the standard. Metric units follow in (parenthesis). In cases when a given formula is traditionally calculated in metric units, for mathematical correctness, it is presented in that manner. NOTE: The Ares vehicles are a preliminary design configuration and will be subject to change as the design progresses. The information in this document was accurate as of the original publication date. Ares Communications Coordinator: Twila Schneider, Marshall Space Flight Center, Schafer Corporation . Ares Communications Strategist: Stephanie Wilson, Marshall Space Flight Center, Schafer Corporation . Writers: John Ristvey, McREL, Dr . Donna Bogner, McREL . Contributing Writer: Deb Aruca, McREL . Graphics: Judy Counley, McREL, Jennie Mitchell, Marshall Space Flight Center . Layout: Lisa Maxfield, McREL . Technical Editor (Original Module): Jacinta Behne, McREL . Editor: Regina Garson, Marshall Space Flight Center . Special thanks to: Kristen Walsh at Boeing for her interview on conducting a launch campaign and launching a rocket . Bob Armstrong and Joel Best from the Marshall Space Flight Center for their interviews on Ares . Special thanks to the following reviewers from NASA’s Marshall Space Flight Center. Melissa Higdon Kristy Hill Bart Leahy Sanda Martel Miranda Martin Dawn Mercer Chuck Pierce Steve Roy Erin Shoemate Mike Wright Additional Reviewers (original module): r D . Gil Yanow, Jet Propulsion Laboratory r D . Dean Eppler, NASA Johnson Space Center Mark Rose, Maplewood Junior/Senior High, PA r D . Donna Bogner, McREL Jacinta Behne, McREL Pat McCartney, McREL This education module, Ares: Launch and Propulsion, was originally developed by educators at Mid-continent Research for Education and Learning (McREL) . iii Ares: Launch and Propulsion: An Educator’s Guide with Activities in Science and Mathematics iv Ares: Launch and Propulsion: An Educator’s Guide with Activities in Science and Mathematics Ares: Launch and Propulsion An Educator’s Guide with Activities in Science and Mathematics Overview: Science Module Introduction In Ares: Launch and Propulsion, students become familiar with how rockets are launched. They also learn how and why specific rockets are chosen for various payloads. This module gives students a hands-on opportunity to experiment with variables that might affect the performance of a launch vehicle. Working in teams, students inves- tigate one variable in detail by performing tests. By completing these tests, students will learn the various aspects involved in launching a rocket. In the assessment, students engage in a competition wherein they apply what they have learned about rockets to build a launch vehicle that flies as high as possible. Curriculum Connections This module contains fourteen hands-on activities for students. Through effective questioning, teachers facilitate students developing awareness of Newton’s Laws of Motion as they apply to rockets. Correlations to National Standards are noted for each activity. Teacher Guide Descriptions Pop Rocket Variables: In this introductory activity, students study the concept of variables in relationship to launching pop rockets. Students will complete a concept map to demonstrate their knowledge of rockets. Pop Goes Newton: Students continue to study the concept of variables in relation to launching pop rockets. The lesson has the students applying each of Newton’s Laws of Motion to the “Pop Rocket Variable” activity. The History of Rocketry: In this activity, students create a multiple tiered timeline on the history of rocketry from ancient times through the Ares Projects. Launching Ares: The student activities in the “Launching Ares” section can be used to create interest in why the Ares missions are critical for returning to the Moon. Students work in groups to determine how to transport construction items and determine the payload and sequence for the transportation. Investigating Water Rockets: In both the abbreviated and comprehensive approach students will get a complete overview of the safety issues with building and launching rockets. Students will complete activities on measuring altitude, fin shape and size, propulsion, and more. Fly Me High: During this performance assessment, students will work in their design groups to design, build, and test launch a water rocket. Students will share their findings with the rest of the class. You Get What You Pay For: This optional activity incorporates an economic component into the module. Students will be given a budget of $150,000 to spend on subcontractors and materials for construction. Role of Student Students will work in teams to learn about various aspects of launching a water rocket related to propulsion. Students will investigate the shape, size, number, and placement of fins, as well as the nose cone shapes. Students then take the information learned in the expert groups back to their design group in order to design and build a water rocket that will fly as high as possible. Overview: Science Module v Ares: Launch and Propulsion: An Educator’s Guide with Activities in Science and Mathematics Multimedia Files NASA Ares I Crew Launch Vehicle: Video with Bob Armstrong . NASA Ares V Cargo Launch Vehicle: Video with Bob Armstrong . Why Two Rockets? Video with Bob Armstrong . Getting Ready for Launch: Video with Joel Best . Why Go to the Moon? Video with Joel Best . Launch Period vs . Launch Window: Audio with Kris Walsh . Mission Integration Managers: Audio with Kris Walsh . The multimedia files were developed especially for this module and are to be used as background information for the teacher and in conjunction with the classroom lessons . They can be downloaded along with the module . The video segments are also available online at: http://www.nasa.gov/mission_pages/constellation/ares/ares_education.html Interaction/Synthesis In this phase of the learning cycle, student/peer interactions are emphasized . These activities contain work to be done in expert groups, with the whole class participating in the safety rules found in the appendices . Once students have had time to explore the rocket variables in these activities, they return to their original design groups to build and test their water rockets . Teachers have two options for implementing this Interaction/Synthesis activity: a comprehensive version in which each design (expert) team studies different variables and a more abbreviated version with fewer variables to inves- tigate, some of which are studied collectively as a class, thereby requiring less class time and teacher preparation . The following synopsis of the two approaches will enable teachers to choose what best meets their needs . Interaction/Synthesis Assessment Comprehensive Approach Abbreviated Approach Safety Rules/Safety Checklist Yes Yes Measuring Altitude Yes Yes Nose Cone Group Yes No (While the nose cone is not tested, it should be constructed for the final assessment) Fin Number and Placement Yes No Fin Shape and Size Yes Yes Volume of Water Yes Yes Individually in expert groups As a class Pressure of Water Yes No Weather or Not Yes No You Get What You Pay For Optional No Fly Me
Load more

Recommended publications
  • Ares I Upper Stage Powering the Second Phase of a Rocket’S Journey to Space
    National Aeronautics and Space Administration NASA’s Ares I Upper Stage Powering the Second Phase of a Rocket’s Journey to Space Going to the moon and beyond will be a stunning Shortly after J-2X engine cutoff, the Orion cap- achievement and an enduring legacy to future sule will separate from the upper stage. Orion’s generations. Supporting the agency’s mission engine then will ignite to insert the capsule into to explore, learn and progress is NASA’s Ares I low-Earth orbit. The Ares I upper stage – dor- crew launch vehicle, an in-line, two-stage rocket. mant after safe shut-down of the J-2X upper The flagship of the Constellation Program’s space stage engine – will re-enter Earth’s atmosphere facts transportation system, the Ares I will carry the and splash down in the Indian Ocean. The upper Orion spacecraft and its crew on missions to the stage and J-2X engine will not be reused. International Space Station and then later on to the moon and beyond. Upper Stage Components The entire Ares I vehicle will be 325 feet tall, with Taking the Ares I on the second phase of its jour- a liftoff mass of 2.0 million pounds and payload ney from Earth will be the spacecraft’s second, capacity of 56,200 pounds mass to low Earth or upper, stage, powered by the J-2X engine. orbit for International Space Station missions, Approximately 133 seconds after liftoff, the Ares and 55,600 pounds mass for lunar missions. I upper stage will separate from the vehicle’s first A self-supporting cylindrical structure, the Ares stage, and the J-2X will ignite.
    [Show full text]
  • Human Issues Related to Spacecraft Vibration During Ascent
    Human Issues related to Spacecraft Vibration during Ascent Consultant Report to the Constellation Program Standing Review Board Jonathan B. Clark M.D., M.P.H. Suite NA 425 One Baylor Plaza Baylor College of Medicine Houston TX 77030-3498 1731 Sunset Blvd Houston TX 77005 713 859 1381 281 989 8721 [email protected] [email protected] Opinions expressed herein are those of the author and do not reflect the views of the National Space Biomedical Research Institute (NSBRI), Baylor College of Medicine (BCM), the University of Texas Medical Branch (UTMB), or the National Aeronautics and Space Administration (NASA). Human Issues related to Spacecraft Vibration during Ascent Consultant Report to the Constellation Program Standing Review Board Jonathan B. Clark M.D., M.P.H. Opinions expressed herein are those of the author and do not reflect the views of the National Space Biomedical Research Institute (NSBRI), Baylor College of Medicine (BCM), the University of Texas Medical Branch (UTMB), or the National Aeronautics and Space Administration (NASA). Pogo in Liquid Fueled Rocket Motors The pogo phenomenon, or fuel pump inlet pressure fluctuation/ cavitation due to tuning feed line resonant frequencies was a major concern in the early space program. Pump tests showed that as inlet pressures were reduced toward cavitation, the pump started acting as an amplifier, causing large oscillations in the thrust chamber pressure. As the rocket engine thrust develops, liquid propellant is cyclically forced into the turbopump. This fluctuating fluid pressure is converted into an unintended and variable increase in engine thrust, with the net effect being longitudinal axis vibration that could result in spacecraft structural failure.
    [Show full text]
  • Ares I Can Model by Clicking on Ares Education Program Under Contacts on the Right of the Screen
    VISIT US ON THE WEB National Aeronautics and Space Administration Be sure to ask for parental assistance before get- ting online at <www.nasa.gov/ares>. Click the Ares Education link, on the left of the screen for additional information: • Print a Full-Page Color Poster and Paper Funnel Template. • View Detailed Ramp Assembly Instructions. • Send us an e-mail with comments and pictures of your Ares I Can Model by clicking on Ares Education Program under Contacts on the right of the screen. ARES I CAN MODEL National Aeronautics and Space Administration George C. Marshall Space Flight Center Huntsville, AL 35812 www.nasa.gov/marshall A hands-on project to help learn about and interact with NASA’s Ares I Rocket. www.nasa.gov NP-2009-06-118-MSFC 8-426227 OVERVIEW NASA plans to take humans back to the Moon, and the Ares I Crew Launch Vehicle (CLV) will help them 1 2 3 4 5 6 7 get there. The Ares I rocket is made of several parts: The recipe shows how to make these can groups. 1. Orion Crew Exploration Vehicle (CEV) 2. Instrument Unit (IU)* RECIPE DISPLAY RAMP 3. Core Stage (CS)* 1. Tape a funnel to the top of an upside down can The Human Factors Engineering Team built a ramp 4. Upper Stage Engine (USE) located within the of peppers (The peppers symbolize the propulsion to proudly display the Ares I Can Model. It is a Interstage (IS)* engine “hot zone” of the Orion Crew Exploration V-shaped ramp made of medium-density fiberboard 5.
    [Show full text]
  • Highlights in Space 2010
    International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no.
    [Show full text]
  • The New Vision for Space Exploration
    Constellation The New Vision for Space Exploration Dale Thomas NASA Constellation Program October 2008 The Constellation Program was born from the Constellation’sNASA Authorization Beginnings Act of 2005 which stated…. The Administrator shall establish a program to develop a sustained human presence on the moon, including a robust precursor program to promote exploration, science, commerce and U.S. preeminence in space, and as a stepping stone to future exploration of Mars and other destinations. CONSTELLATION PROJECTS Initial Capability Lunar Capability Orion Altair Ares I Ares V Mission Operations EVA Ground Operations Lunar Surface EVA EXPLORATION ROADMAP 0506 07 08 09 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 LunarLunar OutpostOutpost BuildupBuildup ExplorationExploration andand ScienceScience LunarLunar RoboticsRobotics MissionsMissions CommercialCommercial OrbitalOrbital Transportation ServicesServices forfor ISSISS AresAres II andand OrionOrion DevelopmentDevelopment AltairAltair Lunar LanderLander Development AresAres VV and EarthEarth DepartureDeparture Stage SurfaceSurface SystemsSystems DevelopmentDevelopment ORION: NEXT GENERATION PILOTED SPACECRAFT Human access to Low Earth Orbit … … to the Moon and Mars ORION PROJECT: CREW EXPLORATION VEHICLE Orion will support both space station and moon missions Launch Abort System Orion will support both space stationDesigned and moonto operate missions for up to 210 days in Earth or lunar Designedorbit to operate for up to 210 days in Earth or lunar orbit Designed for lunar
    [Show full text]
  • 19940015753.Pdf
    National Aeronautics and Educational Product Space Administration Teachers I Grades 2-6 I Office of Education and Human Resources Education Division _o N N cO 0 u_ 0 N t_ I ,.-, CO ,4" U O" 0_ _ Z _ 0 0 tM < u Is LIJ I-. _-.q4" W_ O ul ,,_ W;Z. INWel I I,,-. UJ .... 0,. i,-,{ .... u4 uJ I-,- .. IU_ Z_ .1 i ! I i I j | ] ROCKETS Physical Science Teacher's Guide with Activities National Aeronautics and Space Administration Office of Human Resources and Education Education Division This publication is in the Public Domain and is not protected by copyright. Permission is not required for duplication. EP-291 July 1993 Acknowledgments This publication was developed for the National Aeronautics and Space Administra- tion with the assistance of the many educa- tors of the Aerospace Education Services Program, Oklahoma State University. Writer: Gregory L. Vogt, Ed.D. Teaching From Space Program NASA Johnson Space Center Houston, TX Editor: Carla R. Rosenberg Teaching From Space Program NASA Headquarters Washington, DC Table of Contents How To Use This Guide ............................... 1 Activities and Demonstration Matrix ............. 2 Brief History of Rockets ................................ 3 Rocket Principles ......................................... 8 Practical Rocketry ...................................... 12 Activities and Demonstrations .................... 19 Glossary ..................................................... 40 NASA Educational Materials And Suggested Readings .......................... 41 NASA Educational Resources ................... 42 Evaluation Card ..................................... Insert ii How To Use This Guide vehiclesockets arein theexistence.oldest formEarlyofrocketsself-containedwere in use more than two thousand years ago. Over a long and exciting history, rockets have evolved from simple tubes filled with black powder into mighty vehicles capable of launching a spacecraft out into the galaxy.
    [Show full text]
  • Is Arranged So That Students May Organize a Career Plan by Noting
    DOCUMENT RESUME ED 027 212 SE 006 282 By-Peters, Herman J.; And Others Seven Steps to a Career in Space Science and Technology. Ohio State Univ., Columbus. Research Foundation. Spons Agency-National Aeronautics and Space Administration, Washington, D.C. Report No- EP -33 Pub Date 66 Note- 67p. Available from-Superintendent of Documents, Government Printing Office,Washington, D.C. ($0.45). EDRS Price MF-$0.50 HC Not Available from EDRS. Descriptors-*Aerospace Technology, *Careers, Engineering, Instructional Materia:s,*Occupational Information, *Secondary School Science This guidebook, containing ideas andsuggestions to aid the student in making a career choice, includes information about the space industry and aboutcareer opportunities in space science, engineering, and technology. Suggestions forparents, counselors, librarians, and teacherson how to utilize the book are provided. The book is arranged so that students may organizea career plan by noting special references and by utilizing the checklists at the end of eachchapter. It is suggested that the guidebook be usedover an extended period of time. (BC) U.S. DEPARTMENT Of HEALTH, EDUCATION & WELFARE OFFICE Of EDUCATION _ THIS DOCUMENT HAS BEEN REPRODUCED EXACTLY AS RECEIVED FROM THE PERSON OR ORGANIZATION ORIGINATING IT.POINTS Of VIEW OR OPINIONS STATED DO NOT NECESSARILY REPRESENT OFFICIAL OFFICE Of EDUCATION POSITION OR POLICY. vuo untto 0,1 01-1 s.- 1* ...t9ArproldIVN'Ar HIGH SCHOOL EDITION SEVEN STEPS TO A CAREER IN SPACE SCIENCE AND TECHNOLOGY By Herman J. Peters Samuel F. Angus James J. Ves'sells THE OHIO STATE UNIVERSITY In cooperation with THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Through THE OHIO STATE UNIVERSITY RESEARCH FOUNDATION COLUMBUS, OHIO 1966 For sale by the Superintendent of Documents, U.S.
    [Show full text]
  • Annual Report
    The 2008 Annual Report of the International Space Exploration Coordination Group Released March 2009 International Space Exploration Coordination Group (ISECG) – Annual Report:2008 THIS PAGE INTENTIONALLY BLANK 1 International Space Exploration Coordination Group (ISECG) – Annual Report:2008 CONTENTS Introduction …………………………………………………………………………… 4 Part 1: The Role of the ISECG 1.1 Overview …………………………………………………………………………. 6 1.2 Working Groups of the ISECG …………………………………………………… 7 1.2.1 Enhancement of Public Engagement …………………………………………… 7 1.2.2 Establishment of Relationships with Existing International Working Groups …. 7 1.2.3 The International Space Exploration Coordination Tool (INTERSECT) ……. 8 1.2.4 The Space Exploration Interface Standards Working Group (ISWG) ………….. 8 1.2.5 Mapping the Space Exploration Journey ………………………………………... 8 Part 2: Current and Near-Term Activities of ISECG Members 2.1 Low Earth Orbit (LEO) …………………………………………………………… 10 2.1.1 The International Space Station (ISS) …………………………………………… 10 2.1.2 Emerging Government Capabilities …………………………………………….. 10 2.1.3 Emerging Commercial Providers ……………………………………………….. 11 2.2 Beyond LEO – The Moon and Mars ……………………………………………….. 11 2.2.1 Moon ……………………………………………………………………………… 11 2.2.2 Mars ………………………………………………………………………………. 12 Part 3: Progress in 2008 towards Opportunities for Integrated and Collaborative Space Exploration 3.1 Robotic Network Science – The International Lunar Network ……………………… 16 3.2 Joint Development for Robotic Exploration – Mars Sample Return ………………………… 17 3.3 Collaborative
    [Show full text]
  • A Review of Nasa's Exploration
    A REVIEW OF NASA’S EXPLORATION PROGRAM IN TRANSITION: ISSUES FOR CONGRESS AND INDUSTRY HEARING BEFORE THE SUBCOMMITTEE ON SPACE AND AERONAUTICS COMMITTEE ON SCIENCE, SPACE, AND TECHNOLOGY HOUSE OF REPRESENTATIVES ONE HUNDRED TWELFTH CONGRESS FIRST SESSION MARCH 30, 2011 Serial No. 112–8 Printed for the use of the Committee on Science, Space, and Technology ( Available via the World Wide Web: http://science.house.gov U.S. GOVERNMENT PRINTING OFFICE 65–305PDF WASHINGTON : 2011 For sale by the Superintendent of Documents, U.S. Government Printing Office Internet: bookstore.gpo.gov Phone: toll free (866) 512–1800; DC area (202) 512–1800 Fax: (202) 512–2104 Mail: Stop IDCC, Washington, DC 20402–0001 COMMITTEE ON SCIENCE, SPACE, AND TECHNOLOGY HON. RALPH M. HALL, Texas, Chair F. JAMES SENSENBRENNER, JR., EDDIE BERNICE JOHNSON, Texas Wisconsin JERRY F. COSTELLO, Illinois LAMAR S. SMITH, Texas LYNN C. WOOLSEY, California DANA ROHRABACHER, California ZOE LOFGREN, California ROSCOE G. BARTLETT, Maryland DAVID WU, Oregon FRANK D. LUCAS, Oklahoma BRAD MILLER, North Carolina JUDY BIGGERT, Illinois DANIEL LIPINSKI, Illinois W. TODD AKIN, Missouri GABRIELLE GIFFORDS, Arizona RANDY NEUGEBAUER, Texas DONNA F. EDWARDS, Maryland MICHAEL T. MCCAUL, Texas MARCIA L. FUDGE, Ohio PAUL C. BROUN, Georgia BEN R. LUJA´ N, New Mexico SANDY ADAMS, Florida PAUL D. TONKO, New York BENJAMIN QUAYLE, Arizona JERRY MCNERNEY, California CHARLES J. ‘‘CHUCK’’ FLEISCHMANN, JOHN P. SARBANES, Maryland Tennessee TERRI A. SEWELL, Alabama E. SCOTT RIGELL, Virginia FREDERICA S. WILSON, Florida STEVEN M. PALAZZO, Mississippi HANSEN CLARKE, Michigan MO BROOKS, Alabama ANDY HARRIS, Maryland RANDY HULTGREN, Illinois CHIP CRAVAACK, Minnesota LARRY BUCSHON, Indiana DAN BENISHEK, Michigan VACANCY SUBCOMMITTEE ON SPACE AND AERONAUTICS HON.
    [Show full text]
  • Master Class with Douglas Trumbull: Selected Filmography 1 the Higher Learning Staff Curate Digital Resource Packages to Complem
    Master Class with Douglas Trumbull: Selected Filmography The Higher Learning staff curate digital resource packages to complement and offer further context to the topics and themes discussed during the various Higher Learning events held at TIFF Bell Lightbox. These filmographies, bibliographies, and additional resources include works directly related to guest speakers’ work and careers, and provide additional inspirations and topics to consider; these materials are meant to serve as a jumping-off point for further research. Please refer to the event video to see how topics and themes relate to the Higher Learning event. * mentioned or discussed during the master class ^ special effects by Douglas Trumbull Early Special Effects Films (Pre-1968) The Execution of Mary, Queen of Scots. Dir. Alfred Clark, 1895, U.S.A. 1 min. Production Co.: Edison Manufacturing Company. The Vanishing Lady (Escamotage d’une dame au théâtre Robert Houdin). Dir. Georges Méliès, 1896, France. 1 min. Production Co.: Théâtre Robert-Houdin. A Railway Collision. Dir. Walter R. Booth, 1900, U.K. 1 mins. Production Co.: Robert W. Paul. A Trip to the Moon (Le voyage dans la lune). Dir. Georges Méliès, 1902, France. 14 mins. Production Co.: Star-Film. A Trip to Mars. Dir. Ashley Miller, 1910, U.S.A. 5 mins. Production Co.: Edison Manufacturing Company. The Conquest of the Pole (À la conquête de pôle). Dir. Georges Méliès, 1912, France. 33 mins. Production Co.: Star-Film. *Intolerance: Love’s Struggle Throughout the Ages. Dir. D.W. Griffith, 1916, U.S.A. 197 mins. Production Co.: Triangle Film Corporation / Wark Producing. The Ten Commandments.
    [Show full text]
  • FY10 Agency Mission Planning Model Acronyms
    Version 6-11-09 Mission Data Sources Science Mission Directorate (SMD) submit; 5-4-09 Exploration Systems Mission Directorate (ESMD) submit; 6-11-09 Space Operations Mission Directorate (SOMD) submit; 5-27-09 Aeronautics Research Mission Directorate (ARMD) response; 5-28-09 Mission Acronyms & Definitions Mission Directorate Altair-x Lunar descent stage aka: LSAM = Lunar Surface Access Module (x-mission #) ESMD Ares 1 Crew Launch Vehicle (aka CLV) ESMD Ares V Cargo Launch Vehicle (aka CaLV) ESMD Astro-H SXS Instrument (Explorer Program Mission of Opportunity) [JAXA launch] SMD X-Air Estimated number of Aircraft Earth Science Flights SMD X-Bal Estimated number of Scientific Balloon Flights SMD BARREL Balloon Array for RBSP Relativistic Electron Losses (Two balloon campaigns of 20 flights each) SMD CaLV Cargo Launch Vehicle (aka CaLV) ESMD Chndraayn1 Discovery MoO instrument to be flown on Indian satellite Chandraayan [ELV launch] SMD CLARREO Climate Absolute Radiance and Reflectivity Observatory (see ESDS-x below) SMD CLV Crew Launch Vehicle (aka Ares I) ESMD COR-Lx Cosmic Origins Program Large class mission (x-mission #) (Flagship missions to be defined by Decadal Survey) SMD COR-Mx Cosmic Origins Program Medium class mission (x-mission #) SMD dB decibels ARMD DESDynl Deformation, Ecosystem Structure and Dynamics of Ice (see ESDS-x below) SMD Disc-xx Discovery Mission (xx- mission #) SMD ESDS-x Earth Science Decadal Survey Mission (x- mission #) Likely CLARREO and DESDynI first, order TBD SMD EX-xx Explorer mission (class undefined: Could
    [Show full text]
  • Ares V Cargo Launch Vehicle
    National Aeronautics and Space Administration Constellation Program: America’s Fleet of Next-Generation Launch Vehicles The Ares V Cargo Launch Vehicle Planning and early design are under way for hard- NASA’s Constellation Program to carry human ware, propulsion systems and associated techno- explorers back to the moon, and then onward to logies for NASA’s Ares V cargo launch vehicle — the Mars and other destinations in the solar system. “heavy lifter” of America’s next-generation space fleet. The Ares V effort includes multiple hardware and Ares V will serve as NASA’s primary vessel for safe, propulsion element teams at NASA centers and facts reliable delivery of large-scale hardware to space — contractor organizations around the nation, and is from the lunar landing craft and materials for estab- led by the Ares Projects Office at NASA’s Marshall lishing a moon base, to food, fresh water and other Space Flight Center in Huntsville, Ala. These teams staples needed to extend a human presence beyond rely on nearly a half century of NASA spaceflight Earth orbit. experience and aerospace technology advances. Together, they are developing new vehicle hard- Under the goals of NASA’s exploration mission, ware and flight systems and matur ing technologies Ares V is a vital part of the cost-effective space evolved from powerful, proven Saturn rocket and transportation infrastructure being developed by space shuttle propulsion elements and knowledge. NASA Concept image of Ares V in Earth orbit. (NASA MSFC) The versatile, heavy-lifting Ares V is a two-stage, vertically- stacked launch vehicle. It can carry nearly 414,000 pounds (188 metric tons) to low-Earth orbit.
    [Show full text]