DOCSLIB.ORG

Of Space Law

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Of Space Law JOURNAL OF SPACE LAW VOLUME 19, NUMBER 1 1991 JOURNAL OF SPACE LAW A journal devoted to the legal problems arising out of human activities in outer space VOLUME 19 1991 NUMBER 1 EDITORIAL BOARD AND ADVISORS BERGER, HAROLD GALLOWAY, ElLENE Philadelphia, Pennsylvania Washington, D.C. BOCKSTIEGEL, KARL-HEINZ GOEDHUIS, D. Cologne, Germany London, England, BOURELY, MICHEL G. HE, QIZHI Paris, France Beijing, China COCCA, ALDO ARMANDO JASENTULlYANA, NANDASlRI Buenes Aires, Argentina New York, N.Y. DEMBLING, PAUL G. KOPAL, VLADIMIR Washington, D. C. Prague, Czechoslovakia DlEDERIKS-VERSCHOOR, LH. PH. MCDOUGAl., MYRES S. Baarn, Holland New Haven, Comiecticut FASAN, ERNST VERESHCHETlN, V.S. Neunkirchen, Austria Moscow, U.S.S.R. FINCH, EDWARD R., JR. ZANOTTI, ISIDORO New York, N.Y. Washington, D.C. STEPHEN GOROVE, Chairman University, Mississippi All correspondance should be directed to the JOURNAL OF SPACE LAW, University of Mississippi Law Center, University. Mississippi 38677. JOURNAL OF SPACE LAW. The subscription rate for 1991 is $65 (domestic) and $70 (foreign) for two issues. Single issues may be ordered at $36 per issue (postage and handling included). Copyright @ JOURNAL OF SPACE LAW 1991 Suggested abbreviation: J. SPACE L. JOURNAL OF SPACE LAW A journal devoted to the legal problems arising out of human activities in outer space VOLUME 19 1991 NUMBER 1 STUDENT EDITORIAL ASSISTANTS Rbonda G. Davis, ed. Derwin B. Govan, index & brief news ed. Pamela G. Guren Kenneth C. Johnston Alton J. Le Febvre A. Kelly Sessoms Candidates Clark C. Adams Thomas C. Levidiotis FACULTY ADVISER STEPHEN GOROVE All correspondance with reference to this publication should be directed to the JOURNAL OF SPACE LAW, University of Mississippi Law Center, University, Mississippi 38677. JOURNAL OF SPACE LAW. The subscription rate for 1991 is $65 (domestic) and $70 (foreign) for two issues. Single issues may be ordered at $36 per issue (postage and handling included). Copyright @ JOURNAL OF SPACE LAW 1991 Suggested abbreviation: J. SPACE L. JOURNAL OF SPACE LAW A journal devoted to the legal problems arising out of human activities in outer space VOLUME 19 1991 NUMBER 1 CONTENTS ARTICLES The 1986 Challenger Disaster: Legal Ramifications (Paul G. Dembling and Richard C. Walters) ........................... 1 The Commercial Development of Space: The Need for New Treaties (Bin Cheng) .................................................... 17 SPECIAL FEATURES Events of Interest.. ................................................................... .45 A. Past Events ........................................................................ .45 Reports Space Stations: Problems of Jurisdiction and Conflicts of Law (Stephen Gorove) ............................ :................................... .45 The Twenty-Eighth Session of the Scientific and Technical Sub-Committee of the United Nations Committee on the Peaceful Uses of Outer Space, 26 February to 9 March 1991 (Ralph Chipman) ...................................... .53 The Legal Sub-Committee of COPUOS Convenes its Thirtieth Session with Hope of Progress in· the Codification of Space Law (Yvonne Lodico) ............................................ .57 The Spaceplane and the Law (Tanja L. Masson-Zwaan) ......................60 Comments Emerging Law of Outer Space - The Analogy of Maritime Salvage (Harry H. Almond, Jr.) ....................................................... 67 Case Law Transpace Carriers, Inc. v. United States ........................................ 77 Short Accounts Satellite Communications and the European Community (Katherine M. Gorove) ........................................... 77 The Moon and Mars Missions: Can International Law Meet the Challenge? (Katherine M. Gorove) ........................79 AIAA Technical Committee on Legal Aspects of Aeronautics and Astronautics TC Annual Meeting, May 2, 1990 (William D. Eng /ish) ......................................................... 81 Other Events ................................................................................... 83 B riel News ...................................................................................... 8 3 B. Forthcoming Events ............................................................ 86 Book Reviews/Notices Rarr, Michael & Kohli Rajiv, Commercial Utilization of Space, An International Comparison of Framework Conditions .... 87 Johnson-Freese, Joan, Changing Patterns of International Cooperation in Space .......................................................... 8 7 Sietzen, Frank Jr., World Guide to Commercial Launch Vehicles .... 88 NAS A Thesaurus ............................................................................ 88 Recent Publications . Books ............................................................................................... 89 Contributions to Books .................................................................... 8 9 Articles ...........................................................................................90 Reports ............................................................................................91 Notes/Comments ..............................................................................92 Short Accounts ................................................................................ 92 Book ReviewsIN otices ...................................................................... 92 Official Publications ....................................................................... 93 Cases ...................................... ;......................................................... 96 Miscellaneous ..................................................................................96 Current Documents I. Senate Joint Resolution on the 1992 International Space Year ... l00 II. President Bush's Policy Decision of March 8, 1990, on his Space Exploration Initiative of July 20, 1989 ................... 101 THE 1986 CHALLENGER DISASTER: LEGAL RAMIFICATIONS Paul G. Dembling* and Richard C. Walters" The 1986 Challenger (Shuttle) Disaster, quite aside from the horror and personal tragedy it created, raised distinct legal ramifications which are worthy of analysis and comment. The Disaster deserves special study and attention in terms of the role it has, or might have, played in the continuing evolution of two theories or doctrines which govern the extent to which tort liability is imposed on the federal Government and the private concerns which work under contract to serve the Government's needs. The first is the so-called "F eres doctrine" and the second is the "Government contractor defense." As in most cases, a clear understanding of the operative facts is crucial to an appreciation of their legal import. Background On January 28, 1986,1 an explosion destroyed the Space Shuttle Challenger on its Flight 51-L seventy-three seconds after the liftoff from the Kennedy Space Center, Florida. Seven astronauts were killed. Among these were two military personnel, three employees of the National Aeronautics and Space Administration ("NASA"), and two non-Government . civilians, one of whom was Christa McAuliffe, who was to be the "first teacher in space." A report issued on June 6, 1986 by an independent commission appointed by President Reagan to investigate the accident (commonly known as the "Rogers Commission") concluded that the cause of the accident was a failure in the seal of the joint (the so-called "O-Ring") situated between two segments of the right Solid Rocket Motor ("SRM"). According to the report, hot gases escaped through a leak in the joint's seal and caused the explosion which had destroyed the Challenger. The joint failure, the Commission found, was due to a "faulty design U1lacceptably sensitive to a number of factors [including] temperature, physical '" Partner. Schnader. Harrison, Segal and Lewis, Washington. D.C.; former General Counsel of NASA and the General Accounting Office; member, Editorial Board. JOURNAL OF SPACE LAW. .. Senior Attorney, Schnader, Harrison, Segal and Lewis. Washington, D.C . 1 Ironically, the Apollo fire which caused the death of three astronauts (Grissom, Chaffee, and White) occurred on January 27, 1967. 1 2 JOURNAL OF SPACE LAW Vol. 19, No.1. dimensions, the character of materials, the effects of reusability, processing, and the reaction of the joint to dynamic loading.:'2 "The Commission also determined that a contributing cause of the accident was NASA's decision to proceed with the launch notwithstanding unusually cold temperatures, which affected the joint's ability to seal itself, and despite warnings from engineers at Morton Thiokol, Inc. ("MTI"), the company which had designed and furnished the SRM in question. In its 1988 opinion, the United States District Court for· the Northern District of Utah stated, in the lawsuit instituted by one of the. MTI engineers who warned the company, as fOllows: [The Commission concluded] that the process by which that [NASA] decision was reached within NASA's complex decision-making hierarchy was itself flawed. It found that engineers at MTI, including Roger Boisjoly, were concerned with the performance of the seals in SRM joints at the predicted temperatures. Prior flights launched at significantly warmer temperatures had experienced incomplete seals and minor gas escapes. The engineers made their concerns known to MTI management and to those NASA officials directly involved with the SRM aspect of the Shuttle Program. MTI management initially recommended to NASA officials that the launch
Load more

Recommended publications
  • SPACE RESEARCH in POLAND Report to COMMITTEE
    SPACE RESEARCH IN POLAND Report to COMMITTEE ON SPACE RESEARCH (COSPAR) 2020 Space Research Centre Polish Academy of Sciences and The Committee on Space and Satellite Research PAS Report to COMMITTEE ON SPACE RESEARCH (COSPAR) ISBN 978-83-89439-04-8 First edition © Copyright by Space Research Centre Polish Academy of Sciences and The Committee on Space and Satellite Research PAS Warsaw, 2020 Editor: Iwona Stanisławska, Aneta Popowska Report to COSPAR 2020 1 SATELLITE GEODESY Space Research in Poland 3 1. SATELLITE GEODESY Compiled by Mariusz Figurski, Grzegorz Nykiel, Paweł Wielgosz, and Anna Krypiak-Gregorczyk Introduction This part of the Polish National Report concerns research on Satellite Geodesy performed in Poland from 2018 to 2020. The activity of the Polish institutions in the field of satellite geodesy and navigation are focused on the several main fields: • global and regional GPS and SLR measurements in the frame of International GNSS Service (IGS), International Laser Ranging Service (ILRS), International Earth Rotation and Reference Systems Service (IERS), European Reference Frame Permanent Network (EPN), • Polish geodetic permanent network – ASG-EUPOS, • modeling of ionosphere and troposphere, • practical utilization of satellite methods in local geodetic applications, • geodynamic study, • metrological control of Global Navigation Satellite System (GNSS) equipment, • use of gravimetric satellite missions, • application of GNSS in overland, maritime and air navigation, • multi-GNSS application in geodetic studies. Report
    [Show full text]
  • Leviathan Leviathan
    Leviathan™ st Low Cost Heavy Lift for the 21 Century™ Approved For Public Distribution - Copyright © 2011, DIRECT - All Rights Reserved Leviathan™ st Low Cost Heavy Lift for the 21 Century™ ™ The centerpiece of DIRECT ’s new fleet of space systems, Leviathan™, is a brand-new breed of low cost commercial heavy lift launch vehicle. It is specifically designed to provide unrivaled performance at a price that will finally enable affordable industrial access to space. Leviathan™ With a Payload Fairing diameter of 13.80 meters and a payload capacity over 140 metric tons, Leviathan™ is significantly larger than any other launch vehicle in history, including the Saturn-V rocket that once took astronauts to the moon. Nation / Vehicle Mission Reliability Launch Cost† LEO Payload† Cost / kg to LEO Space Shuttle 130 of 132 (98.48%) $850 million 24,400 kg $34,836 Delta-IV Heavy 13 of 14 (92.86%) $265 million 23,040 kg $11,502 Atlas-V 552 22 of 23 (95.65%) $190 million 20,050 kg $9,476 Ariane-V ES 51.55 (92.73%) $120 million 21,000 kg $5,714 Falcon-9 <Insufficient Data> $56 million 10,450 kg $5,359 Long March 2E 112 of 122 (91.80%) $55 million 14,100 kg $3,901 Proton-M 294 of 335 (87.76%) $80 million 21,000 kg $3,810 Leviathan™ 98.00% * $60 million * 140,000 kg * $429 * * Initial Estimates based on 6 flights per year † Based on publicly available information Leviathan™ is designed to be fully reusable (except the payload fairings) with a minimum of inspections and maintenance between flights.
    [Show full text]
  • FCC-20-54A1.Pdf
    Federal Communications Commission FCC 20-54 Before the Federal Communications Commission Washington, D.C. 20554 In the Matter of ) ) Mitigation of Orbital Debris in the New Space Age ) IB Docket No. 18-313 ) REPORT AND ORDER AND FURTHER NOTICE OF PROPOSED RULEMAKING Adopted: April 23, 2020 Released: April 24, 2020 By the Commission: Chairman Pai and Commissioners O’Rielly, Carr, and Starks issuing separate statements; Commissioner Rosenworcel concurring and issuing a statement. Comment Date: (45 days after date of publication in the Federal Register). Reply Comment Date: (75 days after date of publication in the Federal Register). TABLE OF CONTENTS Heading Paragraph # I. INTRODUCTION .................................................................................................................................. 1 II. BACKGROUND .................................................................................................................................... 3 III. DISCUSSION ...................................................................................................................................... 14 A. Regulatory Approach to Mitigation of Orbital Debris ................................................................... 15 1. FCC Statutory Authority Regarding Orbital Debris ................................................................ 15 2. Relationship with Other U.S. Government Activities ............................................................. 20 3. Economic Considerations .......................................................................................................
    [Show full text]
  • Nasa X-15 Program
    5 24,132 6 9 NASA X-15 PROGRAM By: T.D. Barnes - NASA Contractor - 1960s NASA contractors for the X-15 program were Bendix Field Engineering followed by Unitec, Inc. The NASA High Range Tracking stations were located at Ely and Beatty Nevada with main control being at Dryden/Edwards AFB in California. Personnel at the tracking stations consisted of a Station Manager, a Technical Advisor, and field engineers for the Mod-2 Radar, Data Transmission System, Communications, Telemetry, and Plant Maintenance/Generators. NASA had a site monitor at each tracking station to monitor our contractor operations. Though supporting flights of the X-15 was their main objective, they also participated in flights of the XB-70, the three Lifting Bodies, experimental Lunar Landing vehicles, and an occasional A-12/YF-12/SR-71 Blackbird flight. On mission days a NASA van picked up each member of the crew at their residence for the 4:20 a.m. trip to the tracking station 18 miles North of Beatty on the Tonopah Highway. Upon arrival each performed preflight calibrations and setup of their various systems. The liftoff of the B-52, with the X-15 tucked beneath its wing, seldom occurred after 9:00 a.m. due to the heat effect of the Mojave Desert making it difficult for the planes to acquire altitude. At approximately 0800 hours two pilots from Dryden would proceed uprange to evaluate the condition of the dry lake beds in the event of an emergency landing of the X-15 (always buzzing our station on the way up and back).
    [Show full text]
  • Print Media Portrayal of the Culture of NASA Before and After the Challenger Explosion
    University of Tennessee, Knoxville TRACE: Tennessee Research and Creative Exchange Masters Theses Graduate School 12-2002 Print Media Portrayal of the Culture of NASA Before and After the Challenger Explosion Jodi M. Lockaby University of Tennessee - Knoxville Follow this and additional works at: https://trace.tennessee.edu/utk_gradthes Part of the Communication Commons Recommended Citation Lockaby, Jodi M., "Print Media Portrayal of the Culture of NASA Before and After the Challenger Explosion. " Master's Thesis, University of Tennessee, 2002. https://trace.tennessee.edu/utk_gradthes/3540 This Thesis is brought to you for free and open access by the Graduate School at TRACE: Tennessee Research and Creative Exchange. It has been accepted for inclusion in Masters Theses by an authorized administrator of TRACE: Tennessee Research and Creative Exchange. For more information, please contact [email protected]. To the Graduate Council: I am submitting herewith a thesis written by Jodi M. Lockaby entitled "Print Media Portrayal of the Culture of NASA Before and After the Challenger Explosion." I have examined the final electronic copy of this thesis for form and content and recommend that it be accepted in partial fulfillment of the equirr ements for the degree of Master of Science, with a major in Communication. Mark Littmann, Major Professor We have read this thesis and recommend its acceptance: Bonnie Riechert, John Haas Accepted for the Council: Carolyn R. Hodges Vice Provost and Dean of the Graduate School (Original signatures are on file with official studentecor r ds.) To the Graduate Council: I am submitting herewith a thesis written by Jodi M.
    [Show full text]
  • Space Industry Bulletin July 2019
    VOLUME 2 • ISSUE 7 www.spaceindustrybulletin.com Space Industry Bulletin Market analysis and business intelligence for the space community Commercialising LEO will need destinations beyond the ISS ommercialisation of low investors. And it will depend on and a few private companies Earth orbit will require having destinations beyond just does not make a sustainable in - Cnew models for public- the International Space Station. frastructure. So how do we build private partnership, and it will be For almost two decades, the this community? built on a technology infras- ISS has been the sole hub for Kerry Timmons, LEO com - tructure that will include the commercialisation activities, pro - mercial programme manage - CONTENTS likes of robotics and machine viding unique access to research ment lead at Lockheed Martin learning. and development in a micro- Space, said: “It requires collab - Industry news 2 But commercial success will gravity environment. oration. It needs ‘old space’ and l Virgin Galactic to go public hinge on an infrastructure that Doug Comstock, deputy chief ‘new space’ working in partner - following merger “buys down the risk” for financial officer for integration ship. It needs the commercial l Launch of balloon marks the commercial partners and at NASA, said: “The ISS has 14 market to be energised to bring beginning of a new space era different facilities built by 11 dif - their money and ideas to space.” l Innovation loans offer a share of ferent companies. We don’t want When we talk about commer - £10m funding a gap in capability for human cialising LEO, it’s important to l Galileo outage helps build the access to LEO.” recognise that space is not the case for sovereign UK GNSS Along with destinations, suc - first frontier, and also that Earth l OneWeb takes sustainability into cessful commercialisation of LEO imagery is an industry success orbit and calls on the wider industry will depend on a community, story.
    [Show full text]
  • Beyond the Paths of Heaven the Emergence of Space Power Thought
    Beyond the Paths of Heaven The Emergence of Space Power Thought A Comprehensive Anthology of Space-Related Master’s Research Produced by the School of Advanced Airpower Studies Edited by Bruce M. DeBlois, Colonel, USAF Professor of Air and Space Technology Air University Press Maxwell Air Force Base, Alabama September 1999 Library of Congress Cataloging-in-Publication Data Beyond the paths of heaven : the emergence of space power thought : a comprehensive anthology of space-related master’s research / edited by Bruce M. DeBlois. p. cm. Includes bibliographical references and index. 1. Astronautics, Military. 2. Astronautics, Military—United States. 3. Space Warfare. 4. Air University (U.S.). Air Command and Staff College. School of Advanced Airpower Studies- -Dissertations. I. Deblois, Bruce M., 1957- UG1520.B48 1999 99-35729 358’ .8—dc21 CIP ISBN 1-58566-067-1 Disclaimer Opinions, conclusions, and recommendations expressed or implied within are solely those of the authors and do not necessarily represent the views of Air University, the United States Air Force, the Department of Defense, or any other US government agency. Cleared for public release: distribution unlimited. ii Contents Chapter Page DISCLAIMER . ii OVERVIEW . ix PART I Space Organization, Doctrine, and Architecture 1 An Aerospace Strategy for an Aerospace Nation . 3 Stephen E. Wright 2 After the Gulf War: Balancing Space Power’s Development . 63 Frank Gallegos 3 Blueprints for the Future: Comparing National Security Space Architectures . 103 Christian C. Daehnick PART II Sanctuary/Survivability Perspectives 4 Safe Heavens: Military Strategy and Space Sanctuary . 185 David W. Ziegler PART III Space Control Perspectives 5 Counterspace Operations for Information Dominance .
    [Show full text]
  • 1 American Institute of Aeronautics and Astronautics from Air Bubbles Cast in the Fuel (Voids) Can Cause Problems During Hot-Fire Operations
    Genetic Algorithm Optimization of a Cost Competitive Hybrid Rocket Booster George Story1 NASA MSFC Huntsville, Al Performance, reliability and cost have always been drivers in the rocket business. Hybrid rockets have been late entries into the launch business due to substantial early development work on liquid rockets and solid rockets. Slowly the technology readiness level of hybrids has been increasing due to various large scale testing and flight tests of hybrid rockets. One remaining issue is the cost of hybrids vs the existing launch propulsion systems. This paper will review the known state-of-the-art hybrid development work to date and incorporate it into a genetic algorithm to optimize the configuration based on various parameters. A cost module will be incorporated to the code based on the weights of the components. The design will be optimized on meeting the performance requirements at the lowest cost. I. Introduction Hybrids, considered part solid and part liquid propulsion system, have been caught in the middle of development goals of the various NASA and military programs. Solid rocket motor technology has matured due to the design simplicity, on-demand operational characteristics and low cost. The reliability of solids, given minimal maintenance requirements, made them the ideal system for military applications. On the other hand, liquid rocket engine technology has matured due to their higher specific impulse (ISP) over solids and variable control thrust capability. Hybrid Rockets have been used in only one flight-production application (Teledyne Ryan AQM-81A ‘Firebolt Supersonic Aerial Target) and one series of recent manned flight demonstrations (Burt Rutan’s SpaceshipOne), suggesting that advantages have been overlooked in some potential applications.
    [Show full text]
  • 2015 Year in Review
    National Aeronautics and Space Administration Volume 12 Issue 1 January 2016 2015 Year in Review www.nasa.gov GoddardView Trending – 2 Celebrating Hubble’s 25 Years of Endless Discoveries – 3 Journey to Mars Is More Than Just Fiction – 4 On Earth Day, Rock Stars and Earth Science Share Center Stage – 5 Goddard’s 2015 Milestones NASA Observes Annual at a Glance – 6 Day of Remembrance The Day of Remembrance honors Open Houses Provide a Closer Look members of the NASA family who gave Into NASA’s Work – 8 their lives in the name of exploration. A Scientifically Enlightening Year This year marks the 30th anniversary of in Heliophysics – 10 the Challenger disaster, which claimed Half a Century Later, Rick Obenschain the lives of all seven crew members. Completes His Final NASA Mission – 11 Goddard Honors Sen. Mikulski and Her U.S. Senator From Florida Astronomical Contributions – 12 Tours Goddard’s Facilities Sen. Bill Nelson toured the center’s facilities on Jan. 16. In 1986, as a On the cover: Select Goddard milestones member of the U.S. House of Rep- and accomplishments from 2015. resentatives, Nelson served as a payload specialist during a mission Cover credit: NASA/Goddard/John W. aboard the space shuttle Columbia. Jones NP-2016-1-385-GSFC 2015 Is Warmest Year on Record Independent analyses by the Goddard Institute for Space Studies and the Na- Info tional Oceanic and Atmospheric Admin- istration concluded that Earth’s globally Goddard View is an official publication of averaged surface temperatures in 2015 NASA’s Goddard Space Flight Center in were the warmest since modern record- Greenbelt, Maryland.
    [Show full text]
  • Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
    Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber.
    [Show full text]
  • Sg423finalreport.Pdf
    Notice: The cosmic study or position paper that is the subject of this report was approved by the Board of Trustees of the International Academy of Astronautics (IAA). Any opinions, findings, conclusions, or recommendations expressed in this report are those of the authors and do not necessarily reflect the views of the sponsoring or funding organizations. For more information about the International Academy of Astronautics, visit the IAA home page at www.iaaweb.org. Copyright 2019 by the International Academy of Astronautics. All rights reserved. The International Academy of Astronautics (IAA), an independent nongovernmental organization recognized by the United Nations, was founded in 1960. The purposes of the IAA are to foster the development of astronautics for peaceful purposes, to recognize individuals who have distinguished themselves in areas related to astronautics, and to provide a program through which the membership can contribute to international endeavours and cooperation in the advancement of aerospace activities. © International Academy of Astronautics (IAA) May 2019. This publication is protected by copyright. The information it contains cannot be reproduced without written authorization. Title: A Handbook for Post-Mission Disposal of Satellites Less Than 100 kg Editors: Darren McKnight and Rei Kawashima International Academy of Astronautics 6 rue Galilée, Po Box 1268-16, 75766 Paris Cedex 16, France www.iaaweb.org ISBN/EAN IAA : 978-2-917761-68-7 Cover Illustration: credit A Handbook for Post-Mission Disposal of Satellites
    [Show full text]
  • Clark, Carl Proceedings Sub 2.Pmd
    2015 HAWAII UNIVERSITY INTERNATIONAL CONFERENCES ARTS, HUMANITIES, SOCIAL SCIENCES & EDUCATION JANUARY 03 - 06, 2015 ALA MOANA HOTEL, HONOLULU, HAWAII THE TELL TALE TELLING: AN ANALYSIS OF THE FILM THE CHALLENGER DISASTER TO THE OFFICIAL FINDINGS AND PERSONAL ACCOUNT OF COMMISSION MEMBER DR. FEYNMAN CLARK, CARL WESTLY TEXAS STATE UNIVERSITY COLLEGE MASS COMMUNICATION Mr. Carl Westly Clark Mass Communication Texas State University College. The Tell Tale Telling: An Analysis of the Film The Challenger Disaster to the Official Findings and Personal Account of Commission Member Dr. Feynman A qualitative comparison of the book What do You Care What Other People Think (Feynman and Leighton 1988) and the film The Challenger Disaster (Discovery Science Channel 2013) . Using the cultivation analysis theory to understand the differences in the two narratives and their possible effects on viewer's opinions. The Tell Tale Telling: An analysis of the film The Challenger Disaster to the official findings and personal account of commission member Dr. Feynman By Carl Clark 2014 “Science teaches us what the rules of evidence are. We mess with that at our peril.” William Hurt as Dr. Richard Feynman “For a successful technology, reality must take precedence over public relations, for nature cannot be fooled” Appendix F by Dr. Richard Feynman Abstract The film The Challenger Disaster (Discovery Science Channel 2013) based off of the book by Dr. Richard Feynman What do You Care What Other People Think (Feynman and Leighton 1988) portrays the investigation into the loss of the space shuttle Challenger. The film’s narrative centers on one man against the corruption and special interests of NASA and Washington D.C.
    [Show full text]