Moon Mania! (Now Everyone’S Going There)
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Spaceflight a British Interplanetary Society Publication
SpaceFlight A British Interplanetary Society publication Volume 61 No.2 February 2019 £5.25 Sun-skimmer phones home Rolex in space Skyrora soars ESA uploads 02> to the ISS 634089 From polar platform 770038 to free-flier 9 CONTENTS Features 18 Satellites, lightning trackers and space robots Space historian Gerard van de Haar FBIS has researched the plethora of European payloads carried to the International Space Station by SpaceX Dragon capsules. He describes the wide range of scientific and technical experiments 4 supporting a wide range of research initiatives. Letter from the Editor 24 In search of a role Without specific planning, this Former scientist and spacecraft engineer Dr Bob issue responds to an influx of Parkinson MBE, FBIS takes us back to the news about unmanned space vehicles departing, dying out and origins of the International Space Station and arriving at their intended explains his own role in helping to bring about a destinations. Pretty exciting stuff British contribution – only to see it migrate to an – except the dying bit because it unmanned environmental monitoring platform. appears that Opportunity, roving around Mars for more than 14 30 Shake, rattle and Rolex 18 years, has finally succumbed to a On the 100th anniversary of the company’s birth, global dust storm. Philip Corneille traces the international story Some 12 pages of this issue are behind a range of Rolex watches used by concerned with aspects of the astronauts and cosmonauts in training and in International Space Station, now well into its stride as a research space, plus one that made it to the Moon. -
Exploring the Concept of a Deep Space Solar-Powered Small
EXPLORING THE CONCEPT OF A DEEP SPACE SOLAR-POWERED SMALL SPACECRAFT A Thesis presented to the Faculty of California Polytechnic State University, San Luis Obispo In Partial Fulfillment of the Requirements for the Degree Master of Science in Aerospace Engineering by Kian Crowley June 2018 c 2018 Kian Crowley ALL RIGHTS RESERVED ii COMMITTEE MEMBERSHIP TITLE: Exploring the Concept of a Deep Space Solar-Powered Small Spacecraft AUTHOR: Kian Crowley DATE SUBMITTED: June 2018 COMMITTEE CHAIR: Jordi Puig-Suari, Ph.D. Professor of Aerospace Engineering COMMITTEE MEMBER: Amelia Greig, Ph.D. Assistant Professor of Aerospace Engineering COMMITTEE MEMBER: Kira Abercromby, Ph.D. Associate Professor of Aerospace Engineering COMMITTEE MEMBER: Robert Staehle Jet Propulsion Laboratory iii ABSTRACT Exploring the Concept of a Deep Space Solar-Powered Small Spacecraft Kian Crowley New Horizons, Voyager 1 & 2, and Pioneer 10 & 11 are the only spacecraft to ever venture past Pluto and provide information about space at those large distances. These spacecraft were very expensive and primarily designed to study planets during gravitational assist maneuvers. They were not designed to explore space past Pluto and their study of this environment is at best a secondary mission. These spacecraft rely on radioisotope thermoelectric generators (RTGs) to provide power, an expensive yet necessary approach to generating sufficient power. With Cubesats graduating to interplanetary capabilities, such as the Mars-bound MarCO spacecraft[1], matching the modest payload requirements to study the outer Solar System (OSS) with the capabilities of low-power nano-satellites may enable much more affordable access to deep space. This paper explores a design concept for a low-cost, small spacecraft, designed to study the OSS and satisfy mission requirements with solar power. -
Analytics Manual
ANALYTICS MANUAL August ’09 Analytics Explorers Creating Basic Reports Report Management Custom Reports Dashboards Enterprise Analytics RightNow Documentation Administrators Staff Members Administrator Manual User Manual Navigation Sets System Configuration CTI Administration Common Functionality Staff Management Communication Configuration Screen Pop Contacts Workspaces/Workflows Monetary Configuration Contact Upload Organizations Agent Scripting Database Administration Add-Ins Tasks Customizable Menus External Suppression List Notifications RightNow Business Rules Multiple Interfaces CTI Solution Custom Fields Outlook Integration Configuration Outlook Integration Administrators Staff Members Admins & Designers Service Administrator Service User Manual Customer Portal Manual Incidents Configuring RightNow for Answers Customer Portal Content Library RightNow Chat Configuration RightNow Chat Setting UP WebDAV and Dreamweaver Guided Assistance Service Level Agreements Cloud Monitor Creating Templates and Pages RightNow Wireless Offer Advisor Administration Offer Advisor Working with Widgets RightNow Incident Archiving Deploying Customer Portal Service RightNow Wireless Migrating to Customer Portal Admins Admins & Staff & Staff Sales Administrator Analytics Manual and User Manual Sales Processes Analytics Explorers Quote Templates Report Management Disconnected Access Configuration Creating Basic Reports RightNow Opportunities RightNow Custom Reports Quotes Dashboards Sales Disconnected Access Analytics Enterprise Analytics Staff Members -
Design of a Scalable Nano University Satellite Bus (Illinisat-2 Bus) Command and Data Handling System and Power System
DESIGN OF A SCALABLE NANO UNIVERSITY SATELLITE BUS (ILLINISAT-2 BUS) COMMAND AND DATA HANDLING SYSTEM AND POWER SYSTEM BY ZIPENG WANG THESIS Submitted in partial fulfillment of the requirements for the degree of Master of Science in Aerospace in the Graduate College of the University of Illinois at Urbana-Champaign, 2018 Urbana, Illinois Adviser: Professor Alexander R. M. Ghosh Professor Gary R. Swenson ABSTRACT IlliniSat-2 bus is the second generation of a general model on which multiple-production of CubeSats are based upon. The IlliniSat-2 bus consists of Command and Data Handling system, Power Generation and Distribution system, Attitude Determination and Control system and Radio system. The IlliniSat-2 is required to be capable of operating a nanosatellite from size 1.5U (10x10x17cm) to 6U (10x22.6x36.6cm) and carrying up to three science payloads. The challenge with IlliniSat-2 bus is the requirement for the wide-range scalability. The major contribution of this work includes the requirements, design, testing, and validation of two parts of the IlliniSat-2 bus systems: Command and Data Handling system and Power Generation and Distribution system. This work also contributes the lessons learned throughout the implementation of the flight hardware. So far, five missions are using IlliniSat-2 bus to carry their science payloads: LAICE, CubeSail, SpaceICE, SASSI^2 and CAPSat. CubeSail satellite was fully constructed and delivery to the launcher on April 12th, 2018. The tentative launch date as of this publication is August 31st, 2018. SpaceICE, SASSI^2 and CAPSat are three missions developed as parts of the NASA Science Mission Directorate’s (SMD) Undergraduate Student Instrument Program (USIP). -
Performance Quantification of Heliogyro Solar Sails Using Structural
PERFORMANCE QUANTIFICATION OF HELIOGYRO SOLAR SAILS USING STRUCTURAL, ATTITUDE, AND ORBITAL DYNAMICS AND CONTROL ANALYSIS by DANIEL VERNON GUERRANT B.S., California Polytechnic State University at San Luis Obispo, 2005 M.S., California Polytechnic State University at San Luis Obispo, 2005 A thesis submitted to the Faculty of the Graduate School of the University of Colorado in partial fulfillment of the requirement for the degree of Doctor of Philosophy Department of Aerospace Engineering Sciences 2015 This thesis entitled: Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis written by Daniel Vernon Guerrant has been approved for the Department of Aerospace Engineering Sciences ________________________________________ Dr. Dale A. Lawrence ________________________________________ Dr. W. Keats Wilkie Date______________ The final copy of this thesis has been examined by the signatories, and we find that both the content and the form meet acceptable presentation standards of scholarly work in the above mentioned discipline. Guerrant, Daniel Vernon (Ph.D., Aerospace Engineering Sciences) Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis Thesis directed by Professor Dale A. Lawrence Solar sails enable or enhance exploration of a variety of destinations both within and without the solar system. The heliogyro solar sail architecture divides the sail into blades spun about a central hub and centrifugally stiffened. The resulting structural mass savings can often double acceleration verses kite-type square sails of the same mass. Pitching the blades collectively and cyclically, similar to a helicopter, creates attitude control moments and vectors thrust. The principal hurdle preventing heliogyros’ implementation is the uncertainty in their dynamics. -
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. -
Programa De Pós-Graduação Em Ecologia Fluxo De
INSTITUTO NACIONAL DE PESQUISAS DA AMAZÔNIA - INPA PROGRAMA DE PÓS-GRADUAÇÃO EM ECOLOGIA FLUXO DE ENERGIA EM TEIAS ALIMENTARES DE ECOSSISTEMAS AQUÁTICOS TROPICAIS: DAS FONTES AUTOTRÓFICAS ATÉ OS GRANDES CONSUMIDORES ECTOTÉRMICOS FRANCISCO VILLAMARÍN Manaus, Amazonas i Agosto, 2016 Page i FRANCISCO VILLAMARÍN FLUXO DE ENERGIA EM TEIAS ALIMENTARES DE ECOSSISTEMAS AQUÁTICOS TROPICAIS: DAS FONTES AUTOTRÓFICAS ATÉ OS GRANDES CONSUMIDORES ECTOTÉRMICOS Orientador: WILLIAM E. MAGNUSSON Tese apresentada ao Instituto Nacional de Pesquisas da Amazônia como parte dos requisitos para obtenção do titulo de Doutor em BIOLOGIA-ECOLOGIA Manaus, Amazonas ii Agosto, 2016 Page ii V715 Villamarín, Francisco Fluxo de energia em teias alimentares de ecossistemas aquáticos tropicais: das fontes autotróficas até os grandes consumidores ectotérmicos / Francisco Villamarín. --- Manaus: [s.n.], 2016. 87 f.: il Tese (Doutorado) --- INPA, Manaus, 2016. Orientador: William E. Magnusson Área de concentração: Ecologia 1. Ecossistema aquático. 2. Teia alimentar. 3. Ecologia. I. Título. CDD 574.52632 iii Page iii Sinopse: Estudou-se o fluxo de energia em teias alimentares de ecossistemas aquáticos tropicais do Território Norte da Austrália e da Amazônia central. Aspectos como alocação de energia para reprodução em um peixe herbívoro-detritívoro e origens da energia e posição trófica de crocodilianos amazônicos foram avaliados. Palavras chave: isótopos estáveis, RNA:DNA, energia, consumidores ectotérmicos iv Page iv Dedicatória Mis abuelas Cecilia y Aída me enseñaron con cariño la importancia de la simplicidad y perseverancia en la vida. A ellas, dedico v Page v Agradecimentos O presente trabalho não seria possível sem o incentivo de todas as pessoas que acreditaram e que, de muitas maneiras, contribuiram sempre para que essa pesquisa seja realizada ao longo de todo esse tempo de Amazônia. -
In Situ Propellant Production: Alternatives for Mars Exploration
https://ntrs.nasa.gov/search.jsp?R=19930008610 2020-03-17T09:20:19+00:00Z mira IN SITU PROPELLANT PRODUCTION: ALTERNATIVES FOR MARS EXPLORATION NASA CR 187192 Report No. SAIC-91/1052 Study No. SAIC 1-120-631-$28 by Michael L. Stancati Mark K. Jacobs Kevin J. Cole John T. Collins Science Applications International Corporation 1515 E. Woodfield Road Schaumburg, IL 60173 for Space Propulsion Technology Division NASA Lewis Research Center Cleveland, Ohio Contract NAS3-25809 "qB" October 1991 lWr_ IIm _ IW i m i!i W m m _ 1p m II mmm I z MI qw II - m_ mm_ h ii m_ i PREFACE This study was completed between May 1990 and April 1991 by members of the Advanced Planntng and Analysis Division of Science Applications International Corporation. The study was sponsored by the Space Propulsion Technology Division of NASA Lewis Research Center, and conducted as a task order under contract number NAS3-25809. SAIC acknowledges the contributions of several reviewers who offered valuable insight and commentary w on recovery of raw materials, in situ processing, and propellant utilization strategies. Dr. Robert L. Ash of Old Dominion University examined our characterization of propellant recovery and processing options, and suggested key areas for technology development and early testing of candidate processes. Mr. James R. French of JRF Engineering Services provided a systems-level critique of the assessment approach and alternative utilization strategies, and reviewed the results of performance trades. Dr. Kumar Ramohaili of the Center for Utilization of Lunar and Planetary Resources at the University of Arizona reviewed the infrastructure assessment approach that we proposed, and offered suggestions on presentation of this material. -
COMPLIANCE IS MANDATORY John C. Stennis Space Center Environmental Resources Document
SCWI-8500-0026-ENV Rev. C November 2012 National Aeronautics and Space Administration John C. Stennis Space Center Stennis Space Center, MS 39529-6000 COMPLIANCE IS MANDATORY John C. Stennis Space Center Environmental Resources Document RELEASED - Printed documents may be obsolete; validate prior to use. Stennis SCWI-8500-0026-ENV C Common Work Number Rev. Effective Date: November 21, 2012 Instruction Review Date: November 21, 2017 Page 2 of 268 Responsible Office: RA02/Environmental Management – Center Operations Directorate SUBJECT: Environmental Resources Document This document was prepared under the Stennis Space Center (SSC) Facility Operating Services Contract for the NASA/SSC Center Operations and Support Directorate in support of the SSC Environmental Management System (EMS). Approval/Concurrence Original Signed by David K. Lorance 11/21/2012 NASA/SSC Environmental Officer Date Document History Log Change/ Change Date Originator/ Phone Description Revision Basic 12.9.2005 Wendy Robinson Initial release. 8-2752 A 01.31.2006 Wendy Robinson Changed the effective date to January 31, 2006 8-2752 throughout the document. Changed the review date to January 31, 2011 to reflect 5 years from the effective date throughout the document. Changed the word “revise” date to “review” date in the header throughout the document. Page i – Added signature section above Document History Log. Page ii - Changed telephone number of contact agency to 2584. B 10.03.2008 Jenette Gordon Reviewed and redlined all sections to reflect regulatory 8-1416 changes per media. The section for Natural Resources was rewritten to incorporate the SSC Integrated Natural Resource Management Plan requirements. Additionally, the effective date was changed to May 30, 2008 throughout the document along with the review date to May 30, 2013 to reflect 5 years from the effective date throughout the document. -
The Moon After Apollo
ICARUS 25, 495-537 (1975) The Moon after Apollo PAROUK EL-BAZ National Air and Space Museum, Smithsonian Institution, Washington, D.G- 20560 Received September 17, 1974 The Apollo missions have gradually increased our knowledge of the Moon's chemistry, age, and mode of formation of its surface features and materials. Apollo 11 and 12 landings proved that mare materials are volcanic rocks that were derived from deep-seated basaltic melts about 3.7 and 3.2 billion years ago, respec- tively. Later missions provided additional information on lunar mare basalts as well as the older, anorthositic, highland rocks. Data on the chemical make-up of returned samples were extended to larger areas of the Moon by orbiting geo- chemical experiments. These have also mapped inhomogeneities in lunar surface chemistry, including radioactive anomalies on both the near and far sides. Lunar samples and photographs indicate that the moon is a well-preserved museum of ancient impact scars. The crust of the Moon, which was formed about 4.6 billion years ago, was subjected to intensive metamorphism by large impacts. Although bombardment continues to the present day, the rate and size of impact- ing bodies were much greater in the first 0.7 billion years of the Moon's history. The last of the large, circular, multiringed basins occurred about 3.9 billion years ago. These basins, many of which show positive gravity anomalies (mascons), were flooded by volcanic basalts during a period of at least 600 million years. In addition to filling the circular basins, more so on the near side than on the far side, the basalts also covered lowlands and circum-basin troughs. -
Celebrate Apollo
National Aeronautics and Space Administration Celebrate Apollo Exploring The Moon, Discovering Earth “…We go into space because whatever mankind must undertake, free men must fully share. … I believe that this nation should commit itself to achieving the goal before this decade is out, of landing a man on the moon and returning him safely to Earth. No single space project in this period will be more exciting, or more impressive to mankind, or more important for the long-range exploration of space; and none will be so difficult or expensive to accomplish …” President John F. Kennedy May 25, 1961 Celebrate Apollo Exploring The Moon, Discovering Earth Less than five months into his new administration, on May 25, 1961, President John F. Kennedy, announced the dramatic and ambitious goal of sending an American safely to the moon before the end of the decade. Coming just three weeks after Mercury astronaut Alan Shepard became the first American in space, Kennedy’s bold challenge that historic spring day set the nation on a journey unparalleled in human history. Just eight years later, on July 20, 1969, Apollo 11 commander Neil Armstrong stepped out of the lunar module, taking “one small step” in the Sea of Tranquility, thus achieving “one giant leap for mankind,” and demonstrating to the world that the collective will of the nation was strong enough to overcome any obstacle. It was an achievement that would be repeated five other times between 1969 and 1972. By the time the Apollo 17 mission ended, 12 astronauts had explored the surface of the moon, and the collective contributions of hundreds of thousands of engineers, scientists, astronauts and employees of NASA served to inspire our nation and the world. -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2017) Publication produced for FAA AST by The Tauri Group under contract. NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY .