SATELLITE NO 名称 近地点km 遠地点km 差km 種別 種別 111

Total Page:16

File Type:pdf, Size:1020Kb

SATELLITE NO 名称 近地点km 遠地点km 差km 種別 種別 111 SATELLITE NO 名称 近地点km 遠地点km 差km 種別 種別 111 XATCOBEO 288 898 610 CUBESAT 92 PW-SAT 291 950 659 CUBESAT 47 E-ST@R 292 1012 720 CUBESAT 57 MASAT 1 292 1009 717 CUBESAT 95 ROBUSTA 292 1021 729 CUBESAT 107 UNICUBESAT GG 292 1034 742 CUBESAT AMATEUR RADIO 49 GOLIAT 293 1004 711 CUBESAT 89 POPACS 1 325 1457 1132 CUBESAT 90 POPACS 2 325 1465 1140 CUBESAT 91 POPACS 3 326 1469 1143 CUBESAT 102 TECHEDSAT-3P 332 348 16 CUBESAT AMATEUR RADIO 52 ISS OBJECT B 376 387 11 CUBESAT 1 STARS-II 383 398 15 CUBESAT 51 ISS OBJECT A 391 400 9 CUBESAT 53 ISS OBJECT C 391 400 9 CUBESAT 97 SENSE SV1 402 502 100 CUBESAT 117 ISS(ZARYA) 413 420 7 CUBESAT 112 CHIBIS-M(RS-39) 438 446 8 AMATEUR RADIO 6 AUBIESAT-1 449 765 316 CUBESAT AMATEUR RADIO 56 M-CUBED&EXP-1 PRIME 450 767 317 CUBESAT AMATEUR RADIO 24 DICE-F 451 772 321 CUBESAT AMATEUR RADIO 25 DICE-Y 451 766 315 CUBESAT AMATEUR RADIO 94 RAX-2 451 768 317 CUBESAT AMATEUR RADIO 69 ORS OBJECT C 491 496 5 CUBESAT 83 ORS OBLECT U 492 503 11 CUBESAT 65 ORS OBJECT AD 493 504 11 CUBESAT 72 ORS OBJECT F 493 503 10 CUBESAT 74 ORS OBJECT H 493 499 6 CUBESAT 62 ORS OBJECT AA 494 504 10 CUBESAT 64 ORS OBJECT AC 494 503 9 CUBESAT AMATEUR RADIO 66 ORS OBJECT AE 494 503 9 CUBESAT 67 ORS OBJECT AF 494 503 9 CUBESAT 71 ORS OBJECT E 494 499 5 CUBESAT 76 ORS OBJECT L 494 503 9 CUBESAT 77 ORS OBJECT M 494 503 9 CUBESAT 81 ORS OBLECT S 494 500 6 CUBESAT 82 ORS OBLECT T 494 504 10 CUBESAT 73 ORS OBJECT G 495 502 7 CUBESAT 78 ORS OBJECT P 495 502 7 CUBESAT 79 ORS OBLECT Q 495 502 7 CUBESAT 84 ORS OBLECT V 495 502 7 CUBESAT 86 ORS OBLECT X 495 502 7 CUBESAT 88 ORS OBLECT Z 495 505 10 CUBESAT 63 ORS OBJECT AB 496 501 5 CUBESAT 68 ORS OBJECT B 496 502 6 CUBESAT AMATEUR RADIO 75 ORS OBJECT K 496 501 5 CUBESAT 80 ORS OBLECT R 496 501 5 CUBESAT 85 ORS OBLECT W 496 502 6 CUBESAT 87 ORS OBLECT Y 496 501 5 CUBESAT 70 ORS OBJECT D 497 502 5 CUBESAT AMATEUR RADIO 98 SENSE SV2 497 503 6 CUBESAT AMATEUR RADIO 131 SEDSAT 1(SO-33) 543 1046 503 CUBESAT AMATEUR RADIO 9 BEESAT-3 552 567 15 CUBESAT AMATEUR RADIO 99 SOMP 552 568 16 CUBESAT AMATEUR RADIO 8 BEESAT-2 553 568 15 CUBESAT 44 DOVE-2 555 578 23 CUBESAT AMATEUR RADIO 5 AIST-2 556 578 22 CUBESAT 22 DELFI-C3(DO-64) 587 605 18 CUBESAT 28 DNEPR OBJECT AC 588 640 52 CUBESAT 37 DNEPR OBJECT S 588 640 52 CUBESAT 38 DNEPR OBJECT T 588 640 52 CUBESAT 39 DNEPR OBJECT U 588 638 50 CUBESAT 30 DNEPR OBJECT AE 592 683 91 CUBESAT 31 DNEPR OBJECT AF 592 683 91 CUBESAT 43 DNEPR OBJECT Z 592 699 107 CUBESAT 137 UNISAT-5 592 641 49 CUBESAT 11 BRITE-PL 593 887 294 CUBESAT 23 DELFI-N3XT 593 780 187 CUBESAT 26 DNEPR OBJECT AA 593 715 122 CUBESAT 27 DNEPR OBJECT AB 593 715 122 CUBESAT 32 DNEPR OBJECT AG 593 700 107 CUBESAT 33 DNEPR OBJECT B 593 683 90 CUBESAT 34 DNEPR OBJECT E 593 797 204 CUBESAT 35 DNEPR OBJECT J 593 731 138 CUBESAT 36 DNEPR OBJECT L 593 747 154 CUBESAT 40 DNEPR OBJECT W 593 686 93 CUBESAT 42 DNEPR OBJECT Y 593 700 107 CUBESAT 45 DOVE-3 593 815 222 CUBESAT 50 GOMX 1 593 818 225 CUBESAT 104 TRITON 1 593 763 170 CUBESAT 110 WNISAT-1 593 849 256 CUBESAT 136 TRITON 1 593 763 170 CUBESAT 128 PRISM 594 618 24 CUBESAT 29 DNEPR OBJECT AD 595 639 44 CUBESAT 41 DNEPR OBJECT X 596 640 44 CUBESAT 3 AAUSAT-II 597 616 19 CUBESAT 115 HAMSAT(VO-52) 598 632 34 CUBESAT 15 COMPASS-1 599 619 20 CUBESAT 96 SEEDS II(CO-66) 602 622 20 CUBESAT 13 CANX-2 605 626 21 CUBESAT 21 CUTE-1.7+APD II(CO-65) 605 626 21 CUBESAT 103 TISAT1 605 626 21 CUBESAT 61 NTS(CANX-6) 607 628 21 CUBESAT 138 UOSAT 2(UO-11) 620 631 11 CUBESAT AMATEUR RADIO 17 CUBEBUG1 626 652 26 CUBESAT 60 NEE-01 PEGASUS 626 652 26 CUBESAT 105 TURKSAT-3USAT 626 652 26 CUBESAT 130 SAUDISAT 1C 628 673 45 CUBESAT 133 STARS 637 656 19 CUBESAT AMATEUR RADIO 14 CAPE 1 642 784 142 CUBESAT 16 CSTB 1 642 760 118 CUBESAT 55 LIBERTAD-1 642 785 143 CUBESAT AMATEUR RADIO 58 MAST 643 776 133 CUBESAT 121 KKS-1 645 660 15 CUBESAT 48 ESTCUBE1 656 670 14 CUBESAT 123 MOZHAYETS(RS-22) 669 686 17 CUBESAT 59 NCUBE-2 675 700 25 CUBESAT 19 CUBESAT XI-V(CO-58) 676 701 25 CUBESAT 108 UWE-1 676 701 25 CUBESAT 113 ECHO(AO-51) 694 815 121 CUBESAT 7 BEESAT 707 716 9 CUBESAT 54 ITUPSAT1 707 720 13 AMATEUR RADIO 101 SWISSCUBE 707 719 12 AMATEUR RADIO 109 UWE-2 707 717 10 AMATEUR RADIO 134 SWISSCUBE 707 719 12 AMATEUR RADIO 4 AAUSAT3 768 787 19 AMATEUR RADIO 10 BRITE-AUSTRIA 768 785 17 AMATEUR RADIO 106 UNIBRITE 769 784 15 AMATEUR RADIO 100 STRAND1 770 784 14 AMATEUR RADIO 122 LUSAT(LO-19) 776 791 15 AMATEUR RADIO 125 PACSAT(AO-16) 777 791 14 AMATEUR RADIO 118 ITAMSAT(IO-26) 785 799 14 AMATEUR RADIO 114 EYESAT-1(AO-27) 786 800 14 AMATEUR RADIO 126 PACSAT(NO-44) 787 796 9 AMATEUR RADIO 119 JAS-2(FO-29) 801 1322 521 AMATEUR RADIO 135 TECHSAT 1B(GO-32) 812 816 4 AMATEUR RADIO 2 AAU CUBESAT 814 827 13 AMATEUR RADIO 12 CANX-1 814 827 13 AMATEUR RADIO 20 CUTE-1(CO-55) 814 828 14 AMATEUR RADIO 46 DTUSAT 814 827 13 AMATEUR RADIO 18 CUBESAT XI-IV(CO-57) 815 829 14 AMATEUR RADIO 93 QUAKESAT 815 828 13 AMATEUR RADIO 120 JUGNU 838 866 28 AMATEUR RADIO 132 SRMSAT 850 867 17 AMATEUR RADIO 116 HOPE-1(HO-68) 1193 1204 11 AMATEUR RADIO 124 OSCAR7(AO-7) 1440 1459 19 AMATEUR RADIO 139 YUBILEINY(RS-30) 1479 1509 30 AMATEUR RADIO 129 RADIO ROSTO(RS-15) 1899 2146 247 AMATEUR RADIO 127 PHASE 3B(AO-10) 4102 35346 31244 AMATEUR RADIO.
Recommended publications
  • A Survey and Assessment of the Capabilities of Cubesats for Earth Observation
    Acta Astronautica 74 (2012) 50–68 Contents lists available at SciVerse ScienceDirect Acta Astronautica journal homepage: www.elsevier.com/locate/actaastro Review A survey and assessment of the capabilities of Cubesats for Earth observation Daniel Selva a,n, David Krejci b a Massachusetts Institute of Technology, Cambridge, MA 02139, USA b Vienna University of Technology, Vienna 1040, Austria article info abstract Article history: In less than a decade, Cubesats have evolved from purely educational tools to a standard Received 2 December 2011 platform for technology demonstration and scientific instrumentation. The use of COTS Accepted 9 December 2011 (Commercial-Off-The-Shelf) components and the ongoing miniaturization of several technologies have already led to scattered instances of missions with promising Keywords: scientific value. Furthermore, advantages in terms of development cost and develop- Cubesats ment time with respect to larger satellites, as well as the possibility of launching several Earth observation satellites dozens of Cubesats with a single rocket launch, have brought forth the potential for University satellites radically new mission architectures consisting of very large constellations or clusters of Systems engineering Cubesats. These architectures promise to combine the temporal resolution of GEO Remote sensing missions with the spatial resolution of LEO missions, thus breaking a traditional trade- Nanosatellites Picosatellites off in Earth observation mission design. This paper assesses the current capabilities of Cubesats with respect to potential employment in Earth observation missions. A thorough review of Cubesat bus technology capabilities is performed, identifying potential limitations and their implications on 17 different Earth observation payload technologies. These results are matched to an exhaustive review of scientific require- ments in the field of Earth observation, assessing the possibilities of Cubesats to cope with the requirements set for each one of 21 measurement categories.
    [Show full text]
  • Orbital Lifetime Predictions
    Orbital LIFETIME PREDICTIONS An ASSESSMENT OF model-based BALLISTIC COEFfiCIENT ESTIMATIONS AND ADJUSTMENT FOR TEMPORAL DRAG co- EFfiCIENT VARIATIONS M.R. HaneVEER MSc Thesis Aerospace Engineering Orbital lifetime predictions An assessment of model-based ballistic coecient estimations and adjustment for temporal drag coecient variations by M.R. Haneveer to obtain the degree of Master of Science at the Delft University of Technology, to be defended publicly on Thursday June 1, 2017 at 14:00 PM. Student number: 4077334 Project duration: September 1, 2016 – June 1, 2017 Thesis committee: Dr. ir. E. N. Doornbos, TU Delft, supervisor Dr. ir. E. J. O. Schrama, TU Delft ir. K. J. Cowan MBA TU Delft An electronic version of this thesis is available at http://repository.tudelft.nl/. Summary Objects in Low Earth Orbit (LEO) experience low levels of drag due to the interaction with the outer layers of Earth’s atmosphere. The atmospheric drag reduces the velocity of the object, resulting in a gradual decrease in altitude. With each decayed kilometer the object enters denser portions of the atmosphere accelerating the orbit decay until eventually the object cannot sustain a stable orbit anymore and either crashes onto Earth’s surface or burns up in its atmosphere. The capability of predicting the time an object stays in orbit, whether that object is space junk or a satellite, allows for an estimate of its orbital lifetime - an estimate satellite op- erators work with to schedule science missions and commercial services, as well as use to prove compliance with international agreements stating no passively controlled object is to orbit in LEO longer than 25 years.
    [Show full text]
  • The Annual Compendium of Commercial Space Transportation: 2012
    Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2012 February 2013 About FAA 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 (2013) 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. • i • Federal Aviation Administration’s Office of Commercial Space Transportation Dear Colleague, 2012 was a very active year for the entire commercial space industry. In addition to all of the dramatic space transportation events, including the first-ever commercial mission flown to and from the International Space Station, the year was also a very busy one from the government’s perspective. It is clear that the level and pace of activity is beginning to increase significantly.
    [Show full text]
  • → Space for Europe European Space Agency
    number 149 | February 2012 bulletin → space for europe European Space Agency The European Space Agency was formed out of, and took over the rights and The ESA headquarters are in Paris. obligations of, the two earlier European space organisations – the European Space Research Organisation (ESRO) and the European Launcher Development The major establishments of ESA are: Organisation (ELDO). The Member States are Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, the ESTEC, Noordwijk, Netherlands. Netherlands, Norway, Portugal, Romania, Spain, Sweden, Switzerland and the United Kingdom. Canada is a Cooperating State. ESOC, Darmstadt, Germany. In the words of its Convention: the purpose of the Agency shall be to provide for ESRIN, Frascati, Italy. and to promote, for exclusively peaceful purposes, cooperation among European States in space research and technology and their space applications, with a view ESAC, Madrid, Spain. to their being used for scientific purposes and for operational space applications systems: Chairman of the Council: D. Williams → by elaborating and implementing a long-term European space policy, by Director General: J.-J. Dordain recommending space objectives to the Member States, and by concerting the policies of the Member States with respect to other national and international organisations and institutions; → by elaborating and implementing activities and programmes in the space field; → by coordinating the European space programme and national programmes, and by integrating the latter progressively and as completely as possible into the European space programme, in particular as regards the development of applications satellites; → by elaborating and implementing the industrial policy appropriate to its programme and by recommending a coherent industrial policy to the Member States.
    [Show full text]
  • Cubesat Communication Systems 2003-2013: a Historical Look
    CubeSat Communication Systems 2003-2013: A Historical Look Bryan Klofas SRI International [email protected] Nanosatellite Ground Station Workshop San Luis Obispo, California 23 April 2013 Two Survey Papers • “A Survey of CubeSat Communication Systems” – Paper presented at the CubeSat Developers’ Workshop 2008 – By Bryan Klofas, Jason Anderson, and Kyle Leveque – Covers the CubeSats from start of program to 2008 • “A Survey of CubeSat Communication Systems: 2009-2012” – Paper presented at the CubeSat Developers’ Workshop 2013 – By Bryan Klofas and Kyle Leveque – Covers the CubeSats from 2009 to ELaNa-6/NROL-36 launch in 2012 Slide 2 Summary of CubeSat Launches 2003 to 2013 • Eurockot (30 June 2003) • Dnepr Launch 2 (17 Apr 2007) – AAU1 CubeSat – CSTB1 – DTUsat-1 – AeroCube-2 – CanX-1 – CP4 – Cute-1 – Libertad-1 – QuakeSat-1 – CAPE1 – XI-IV – CP3 • SSETI Express (27 Oct 2005) – MAST – XI-V • NLS-4/PSLV-C9 (28 Apr 2008) – NCube-2 – Delfi-C3 – UWE-1 – SEEDS-2 • M-V-8 (22 Feb 2006) – CanX-2 – Cute-1.7+APD – AAUSAT-II • Minotaur 1 (11 Dec 2006) – Compass-1 – GeneSat-1 Slide 3 Summary of CubeSat Launches 2003 to 2013 • Minotaur-1 (19 May 2009) • NLS-6/PSLV-C15 (12 July 2010) – AeroCube-3 – Tisat-1 – CP6 – StudSat – HawkSat-1 • STP-S26 (19 Nov 2010) – PharmaSat – RAX-1 • ISILaunch 01 (23 Sep 2009) – O/OREOS – BEESAT-1 – NanoSail-D2 – UWE-2 • Falcon 9-002 (8 Dec 2010) – ITUpSAT-1 – Perseus (4) – SwissCube – QbX (2) • H-IIA F17 (20 May 2010) – SMDC-ONE – Hayato – Mayflower – Waseda-SAT2 – PSLV-C18 (12 Oct 2011) – Negai-Star – Jugnu Slide 4 Summary
    [Show full text]
  • Development of Magnetometer-Based Orbit And
    DEVELOPMENT OF MAGNETOMETER-BASED ORBIT AND ATTITUDE DETERMINATION FOR NANOSATELLITES THOMAS WRIGHT A THESIS SUBMITTED TO THE FACULTY OF GRADUATE STUDIES IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE GRADUATE PROGRAM IN EARTH AND SPACE SCIENCE YORK UNIVERSITY, TORONTO, ONTARIO AUGUST, 2014 © THOMAS WRIGHT, 2014 Abstract Attitude and orbit determination are critical parts of nanosatellite mission operations. The ability to perform attitude and orbit determination autonomously could lead to a wider array of mission possibilities for nanosatellites. This research examines the feasibility of using low-cost magnetometer measurements as a method of autonomous, simultaneous orbit and attitude determination for the novel application of redundancy on nanosatellites. Individual Extended Kalman Filters (EKFs) are developed for both attitude determination and orbit determination. Simulations are run to compare the developed systems with previous work on attitude and orbit determination. The EKFs are combined to provide both attitude and orbit determination simultaneously. Simulations are run and show that this approach for autonomous attitude and orbit determination on nanosatellites provides 8.5 and 12.5 km of attitude and orbit knowledge, respectively. The results of the simulations are then validated using Hardware-In-The-Loop (HITL) testing. Additionally, a Helmholtz cage is evaluated for future use in the HITL test setup. ii Acknowledgements I would like to acknowledge my supervisors Professor Sunil Bisnath and Professor Regina Lee for their guidance and support. I will carry the skills they helped me to develop through the rest of my career. I would also like to thank the grad students in both the GNSS and YuSEND Labs for their assistance and encouragement throughout my studies.
    [Show full text]
  • Future Technologies
    MANEKSHAW PAPER No. 47, 2014 Future Technologies Puneet Bhalla D W LAN ARFA OR RE F S E T R U T D N IE E S C CLAWS VI CT N OR ISIO Y THROUGH V KNOWLEDGE WORLD Centre for Land Warfare Studies KW Publishers Pvt Ltd New Delhi New Delhi Editorial Team Editor-in-Chief : Maj Gen Dhruv C Katoch SM, VSM (Retd) Managing Editor : Ms Avantika Lal D W LAN ARFA OR RE F S E T R U T D N IE E S C CLAWS VI CT N OR ISIO Y THROUGH V Centre for Land Warfare Studies RPSO Complex, Parade Road, Delhi Cantt, New Delhi 110010 Phone: +91.11.25691308 Fax: +91.11.25692347 email: [email protected] website: www.claws.in The Centre for Land Warfare Studies (CLAWS), New Delhi, is an autonomous think tank dealing with national security and conceptual aspects of land warfare, including conventional and sub-conventional conflicts and terrorism. CLAWS conducts research that is futuristic in outlook and policy-oriented in approach. © 2014, Centre for Land Warfare Studies (CLAWS), New Delhi Disclaimer: The contents of this paper are based on the analysis of materials accessed from open sources and are the personal views of the author. The contents, therefore, may not be quoted or cited as representing the views or policy of the Government of India, or Integrated Headquarters of MoD (Army), or the Centre for Land Warfare Studies. KNOWLEDGE WORLD www.kwpub.com Published in India by Kalpana Shukla KW Publishers Pvt Ltd 4676/21, First Floor, Ansari Road, Daryaganj, New Delhi 110002 Phone: +91 11 23263498 / 43528107 email: [email protected] l www.kwpub.com Contents 1.
    [Show full text]
  • Space Security Index 2013
    SPACE SECURITY INDEX 2013 www.spacesecurity.org 10th Edition SPACE SECURITY INDEX 2013 SPACESECURITY.ORG iii Library and Archives Canada Cataloguing in Publications Data Space Security Index 2013 ISBN: 978-1-927802-05-2 FOR PDF version use this © 2013 SPACESECURITY.ORG ISBN: 978-1-927802-05-2 Edited by Cesar Jaramillo Design and layout by Creative Services, University of Waterloo, Waterloo, Ontario, Canada Cover image: Soyuz TMA-07M Spacecraft ISS034-E-010181 (21 Dec. 2012) As the International Space Station and Soyuz TMA-07M spacecraft were making their relative approaches on Dec. 21, one of the Expedition 34 crew members on the orbital outpost captured this photo of the Soyuz. Credit: NASA. Printed in Canada Printer: Pandora Print Shop, Kitchener, Ontario First published October 2013 Please direct enquiries to: Cesar Jaramillo Project Ploughshares 57 Erb Street West Waterloo, Ontario N2L 6C2 Canada Telephone: 519-888-6541, ext. 7708 Fax: 519-888-0018 Email: [email protected] Governance Group Julie Crôteau Foreign Aairs and International Trade Canada Peter Hays Eisenhower Center for Space and Defense Studies Ram Jakhu Institute of Air and Space Law, McGill University Ajey Lele Institute for Defence Studies and Analyses Paul Meyer The Simons Foundation John Siebert Project Ploughshares Ray Williamson Secure World Foundation Advisory Board Richard DalBello Intelsat General Corporation Theresa Hitchens United Nations Institute for Disarmament Research John Logsdon The George Washington University Lucy Stojak HEC Montréal Project Manager Cesar Jaramillo Project Ploughshares Table of Contents TABLE OF CONTENTS TABLE PAGE 1 Acronyms and Abbreviations PAGE 5 Introduction PAGE 9 Acknowledgements PAGE 10 Executive Summary PAGE 23 Theme 1: Condition of the space environment: This theme examines the security and sustainability of the space environment, with an emphasis on space debris; the potential threats posed by near-Earth objects; the allocation of scarce space resources; and the ability to detect, track, identify, and catalog objects in outer space.
    [Show full text]
  • Nanosatelliitide Tehnoloogia Arengutrendid
    View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by DSpace at Tartu University Library TARTU ÜLIKOOL Loodus- ja tehnoloogiateaduskond Füüsika Instituut Erik Kulu Nanosatelliitide tehnoloogia arengutrendid Magistritöö (30 EAP) Juhendaja: Mart Noorma Tartu 2014 SISUKORD 1 Sissejuhatus ........................................................................................................................ 4 2 Metoodika ........................................................................................................................... 6 3 Nanosatelliidid ja nende areng ........................................................................................... 8 3.1 Nanosatelliitide arendamise hetkeseis ....................................................................... 13 3.2 Nanosatelliitide projektide omadused ....................................................................... 16 4 Nanosatelliitide projektide seos haridusega, innovatsiooniga ja teaduse populariseerimisega ................................................................................................................. 18 4.1 Nanosatelliitide hariduslikud aspektid ...................................................................... 18 4.1.1 Hariduslikud projektid ülikoolides .................................................................... 20 4.1.2 Hariduslikud projektid ettevõtetes ..................................................................... 20 4.1.3 Hariduslikud programmid kosmoseagentuurides .............................................
    [Show full text]
  • Istnanosat-1 Quality Assurance, Risk Management and Assembly, Integration and Verification Planning
    ISTNanosat-1 Quality Assurance, Risk Management and Assembly, Integration and Verification Planning Pedro Filipe Rodrigues Coelho Thesis to obtain the Master of Science Degree in Aerospace Engineering Supervisor: Prof. Rui M. Rocha Co-Supervisor: Prof. Moisés S. Piedade Examination Committee Chairperson: Prof. João Miranda Lemos Supervisor: Prof. Rui M. Rocha Co-Supervisor: Prof. Moisés S. Piedade Members of the Committee: Prof. Agostinho A. da Fonseca May 2016 ii Acknowledgments To Professor Rui Rocha and Professor Moisés Piedade, I have to thank the opportunity to work in the ISTNanoSat-1 Project, the guidance throughout the project and the most required pushes for this project conclusion. I would like to thank Laurent Marchand and Nicolas Saillen for the support, drive and belief. It would never have been possible to complete this work without their support and flexibility as well as their drive in my professional endeavors. To all the friendships university brought and endured in my life, that shared the worst and best of university, the late nights of work and study, the challenging exchange of ideas and ideals and all the growing into adulthood. To all my friends in ESA/ESTEC, for filling the best possible work experience with the best personnel environment. Their joy and enthusiasm in work and life were and will always be an inspiration in my life. A lei, bella Annalisa coppia di ballo, per essere la musica e la giola in tutti i76955+ momenti… À minha família, Mãe, Pai e Irmã, pelo amor incondicional, paciência e crença sem limites. Não tenho como retribuir o esforço incansável, todo o carinho e a educação modelar, senão agarrar o futuro pelo qual tanto lutaram comigo.
    [Show full text]
  • A Sample AMS Latex File
    PLEASE SEE CORRECTED APPENDIX A IN CORRIGENDUM, JOSS VOL. 6, NO. 3, DECEMBER 2017 Zea, L. et al. (2016): JoSS, Vol. 5, No. 3, pp. 483–511 (Peer-reviewed article available at www.jossonline.com) www.DeepakPublishing.com www. JoSSonline.com A Methodology for CubeSat Mission Selection Luis Zea, Victor Ayerdi, Sergio Argueta, and Antonio Muñoz Universidad del Valle de Guatemala, Guatemala City, Guatemala Abstract Over 400 CubeSats have been launched during the first 13 years of existence of this 10 cm cube-per unit standard. The CubeSat’s flexibility to use commercial-off-the-shelf (COTS) parts and its standardization of in- terfaces have reduced the cost of developing and operating space systems. This is evident by satellite design projects where at least 95 universities and 18 developing countries have been involved. Although most of these initial projects had the sole mission of demonstrating that a space system could be developed and operated in- house, several others had scientific missions on their own. The selection of said mission is not a trivial process, however, as the cost and benefits of different options need to be carefully assessed. To conduct this analysis in a systematic and scholarly fashion, a methodology based on maximizing the benefits while considering program- matic risk and technical feasibility was developed for the current study. Several potential mission categories, which include remote sensing and space-based research, were analyzed for their technical requirements and fea- sibility to be implemented on CubeSats. The methodology helps compare potential missions based on their rele- vance, risk, required resources, and benefits.
    [Show full text]
  • Small Spacecraft Technology State of the Art
    NASA/TP–2015–216648/REV1 Small Spacecraft Technology State of the Art Mission Design Division Ames Research Center, Moffett Field, California December 2015 NASA STI Program . in Profile Since its founding, NASA has been dedicated • CONFERENCE PUBLICATION. to the advancement of aeronautics and space Collected papers from scientific and science. The NASA scientific and technical technical conferences, symposia, seminars, information (STI) program plays a key part or other meetings sponsored or in helping NASA maintain this important co-sponsored by NASA. role. • SPECIAL PUBLICATION. Scientific, The NASA STI Program operates under the technical, or historical information from auspices of the Agency Chief Information NASA programs, projects, and missions, Officer. It collects, organizes, provides for often concerned with subjects having archiving, and disseminates NASA’s STI. substantial public interest. The NASA STI Program provides access to the NASA Aeronautics and Space Database • TECHNICAL TRANSLATION. English- and its public interface, the NASA Technical language translations of foreign scientific Report Server, thus providing one of the and technical material pertinent to largest collection of aeronautical and space NASA’s mission. science STI in the world. Results are Specialized services also include creating published in both non-NASA channels and custom thesauri, building customized by NASA in the NASA STI Report Series, databases, and organizing and publishing which includes the following report types: research results. • TECHNICAL PUBLICATION. Reports of For more information about the NASA STI completed research or a major significant Program, see the following: phase of research that present the results of NASA programs and include extensive • Access the NASA STI program home page data or theoretical analysis.
    [Show full text]