Canada in Space May 29, 2004
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TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
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. -
2010 Commercial Space Transportation Forecasts
2010 Commercial Space Transportation Forecasts May 2010 FAA Commercial Space Transportation (AST) and the Commercial Space Transportation Advisory Committee (COMSTAC) HQ-101151.INDD 2010 Commercial Space Transportation Forecasts About the 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 49 United States Code, Subtitle IX, Chapter 701 (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 web site at http://ast.faa.gov. Cover: Art by John Sloan (2010) 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 / Commercial Space Transportation Table of Contents Executive Summary . 1 Introduction . 4 About the CoMStAC GSo Forecast . .4 About the FAA NGSo Forecast . .4 ChAracteriStics oF the CommerCiAl Space transportAtioN MArket . .5 Demand ForecastS . .5 COMSTAC 2010 Commercial Geosynchronous Orbit (GSO) Launch Demand Forecast . 7 exeCutive Summary . .7 BackGround . .9 Forecast MethoDoloGy . .9 CoMStAC CommerCiAl GSo Launch Demand Forecast reSultS . -
The Need for Detailed Ionic Composition of the Near-Earth Plasma
HeliophysicsHELIO 2050 2050 White Papers (2021) R. Ilie4094.pdf THE NEED FOR DETAILED IONIC COMPOSITION OF THE NEAR-EARTH PLASMA An impressive body of work has been devoted to the escape of H+, He+ and O+ ions from Earth’s ionosphere, and their circulation and redistribution throughout the terrestrial magneto- sphere (Schunk and Raitt, 1980; Schunk and Sojka, 1997; Winglee et al., 2002; Glocer et al., 2009; Ilie et al., 2015; Ilie and Liemohn, 2016). However, the transport and energization of N+, in addi- tion to that of O+, has not been considered by most studies, even though a number of direct and indirect measurements made to describe the ionic composition of the ionosphere-magnetosphere system, have established that N+ is a significant ion species in the ionosphere and its presence in the magnetosphere is significant. A wide range in the magnitude oftheN+ to O+ density ratio has been reported, with significant variations not only with geomagnetic activity, but also with solar cycle, season, time of day, latitude, etc (Mall et al., 2002; Christon et al., 2002). These vari- ations suggest that N+ and O+, while relatively close in mass, they obey different chemical and energization processes, and possibly follow different paths of energization. In addition, observations from the WIND STICS ISIS 2 spacecraft (Hoffman et al., 1974) indicated that not only N+, but also molecular ions were ob- served in the Earth’s magnetosphere Geotail STICS AMPTE and ionosphere. Measurements from CCE Explorer 31 Akebono SMS the Arase satellite (Miyoshi et al., MMS ISIS-2 IMS DE-1 RIMSS e-POP 2018) showed the existence of molec- OGO-6 OGOGO-2-2 IMSS Sputnik3 IMS AE-C ular ions in the Earth’s ring cur- RMS IMS rent region, even under moderate ge- omagnetic storm conditions. -
Telesat Completes Agreements for Satellite Capacity with Bell TV and Echostar Corporation
Telesat Completes Agreements for Satellite Capacity with Bell TV and EchoStar Corporation Bell TV Commits to Construction of New Canadian Broadcast Satellite and EchoStar Will Use Entire Available Nimiq 5 Payload OTTAWA, Sep. 17, 2009 (Canada NewsWire via COMTEX News Network) -- Telesat, the world's fourth largest fixed satellite services operator, announced today that it has completed agreements for new satellite capacity with two of its key customers, Bell TV and EchoStar Corporation (Nasdaq: SATS). Bell TV, the leading provider of direct-to-home services in Canada, has agreed to utilize a new Telesat direct broadcast satellite which is planned for construction beginning in the first quarter of 2010. The new satellite will augment Bell TV's capacity and capabilities at its prime orbital locations of 82 and 91 degrees West. EchoStar, which had previously contracted for half the capacity of Telesat's new Nimiq 5 satellite, has now committed to use the entire available Nimiq 5 payload for the anticipated 15-year life of the satellite. "We are very pleased to have entered into arrangements that meet the strategic requirements of Bell TV and EchoStar, two longstanding and important Telesat customers," said Dan Goldberg, Telesat's President and CEO. "We look forward to the launch of Nimiq 5 scheduled for later today and beginning construction on the new satellite for Bell TV early next year." Nimiq 5 is scheduled for launch on a Proton rocket September 18th from the Baikonur Cosmodrome in Kazakhstan (September 17th in Ottawa) and is intended to operate in geostationary orbit from 72.7 degrees West. -
Space Systems/Loral Selected to Provide Anik G1 Satellite to Telesat
Space Systems/Loral Selected to Provide Anik G1 Satellite to Telesat Space Systems/Loral Platform Provides Flexibility to Accommodate Multiple Missions PALO ALTO, Calif., Jun 1, 2010 (GlobeNewswire via COMTEX News Network) -- Space Systems/Loral (SS/L), the world's leading provider of commercial satellites, today announced that it has been selected to provide a satellite to Telesat, one of the world's leading satellite operators. The new satellite, Anik G1, is a multi-mission spacecraft that supports a variety of applications including direct-to-home (DTH) television broadcasting in Canada; government requirements over the Americas and the Pacific; and broadband, voice, data and video services in South America. "The Space Systems/Loral platform offered us the flexibility to build on the commitment of a key Telesat customer, Shaw Direct, that will use Anik G1 to expand their video service offerings across Canada," said Dan Goldberg, President and CEO of Telesat. "The ability to cost effectively combine multiple service missions on one satellite makes the SS/L platform a winning solution for Telesat and our customers." Anik G1 is a multi-band satellite that will be located at 107.3 degrees West Longitude when it goes into service in the second half of 2012. The satellite will provide 16 high-power Ku-band transponders in the extended FSS band to support Shaw Direct's growing DTH video programming for the Canadian market. It also has 12 Ku-band and 24 C-band transponders that will both replace and expand on Telesat's Anik F1 satellite now serving South America. In addition, Anik G1 will have three X-band channels for government services over the Americas and part of the Pacific Ocean, and one channel in the reverse Direct Broadcast Service band. -
Polar Topside Ionosphere During Geomagnetic Storms: Comparison
Radio Science RESEARCH ARTICLE Polar Topside Ionosphere During Geomagnetic Storms: 10.1029/2018RS006589 Comparison of ISIS-II With TDIM Special Section: J. J. Sojka1,2 , D. Rice2 , V. Eccles2 , M. David1 , R. W. Schunk1 , R. F. Benson3 , URSI General Assembly and and H. G. James4 Scientific Symposium (2017) 1Center for Atmospheric and Space Sciences, Utah State University, Logan, UT, USA, 2Space Environment Corporation, 3 Key Points: Logan, UT, USA, Geospace Physics Laboratory, Heliophysics Science Division, NASA Goddard Space Flight Center, • The paper focuses on prestorm and Greenbelt, MD, USA, 4Natural Resources Canada Geomagnetic Laboratory, Ottawa, Ontario, Canada main phase topside ionospheric response to a mild and a severe geomagnetic storm Abstract Space weather deposits energy into the high polar latitudes, primarily via Joule heating that is • Simulations from an extensively used associated with the Poynting flux electromagnetic energy flow between the magnetosphere and F region model, TDIM, are compared fl fi to ISIS-II topside ionosphere ionosphere. One way to observe this energy ow is to look at the ionospheric electron density pro le observations (EDP), especially that of the topside. The altitude location of the ionospheric peak provides additional • Surprisingly, the TDIM is unable to information on the net field-aligned vertical transport at high latitudes. To date, there have been few simulate the observed storm response while satisfactorily studies in which physics-based ionospheric model storm simulations have been compared with topside simulating the prestorm topside EDPs. A rich database of high-latitude topside ionograms obtained from polar orbiting satellites of the International Satellites for Ionospheric Studies (ISIS) program exists but has not been utilized in comparisons with physics-based models. -
AUTOMATED NEAR REAL TIME RADARSAT-2 IMAGE GEO-PROCESSING and ITS APPLICATION for SEA ICE and OIL SPILL MONITORING )/,( )/,( Vugy
AUTOMATED NEAR REAL TIME RADARSAT-2 IMAGE GEO-PROCESSING AND ITS APPLICATION FOR SEA ICE AND OIL SPILL MONITORING Ziqiang Ou Canadian Ice Service, Environment Canada 373 Sussex Drive, Ottawa, Canada K1A 0H3 - [email protected] KEY WORDS: RADARSAT, SAR, Georeferencing, Real-time, Pollution, Snow Ice, Detection ABSTRACT: Synthetic aperture radar (SAR) data from RADARSAT-1 are an important operational data source for several ice centres around the world. Sea ice monitoring has been the most successful real-time operational application for RADARSAT-1 data. These data are used by several national ice services as a mainstay of their programs. Most recently, Canadian Ice Service launched another new real-time operational program called ISTOP (Integrated Satellite Tracking Of Pollution). It uses the RADARSAT-1 data to monitor ocean and lakes for oil slicks and tracking the polluters. In this paper, we consider the ice information requirements for operational sea ice monitoring and the oil slick and target detection requirements for operational ISTOP program at the Canadian Ice Service (CIS), and the potential for RADARSAT-2 to meet those requirements. Primary parameters are ice-edge location, ice concentration, and stage of development; secondary parameters include leads, ice thickness, ice topography and roughness, ice decay, and snow properties. Iceberg detection is an additional ice information requirement. The oil slick and ship target detection are the basic requirements for the surveillance and pollution control. 1. INTRODUCTION 2. GEOMETRIC TRANSFORMATION RADARSAT-2 products are provided in a GeoTIFF format There are two major techniques for correcting geometric with a sets of support XML files for all products except the distortion present in an image. -
Federal Register/Vol. 86, No. 91/Thursday, May 13, 2021/Proposed Rules
26262 Federal Register / Vol. 86, No. 91 / Thursday, May 13, 2021 / Proposed Rules FEDERAL COMMUNICATIONS BCPI, Inc., 45 L Street NE, Washington, shown or given to Commission staff COMMISSION DC 20554. Customers may contact BCPI, during ex parte meetings are deemed to Inc. via their website, http:// be written ex parte presentations and 47 CFR Part 1 www.bcpi.com, or call 1–800–378–3160. must be filed consistent with section [MD Docket Nos. 20–105; MD Docket Nos. This document is available in 1.1206(b) of the Commission’s rules. In 21–190; FCC 21–49; FRS 26021] alternative formats (computer diskette, proceedings governed by section 1.49(f) large print, audio record, and braille). of the Commission’s rules or for which Assessment and Collection of Persons with disabilities who need the Commission has made available a Regulatory Fees for Fiscal Year 2021 documents in these formats may contact method of electronic filing, written ex the FCC by email: [email protected] or parte presentations and memoranda AGENCY: Federal Communications phone: 202–418–0530 or TTY: 202–418– summarizing oral ex parte Commission. 0432. Effective March 19, 2020, and presentations, and all attachments ACTION: Notice of proposed rulemaking. until further notice, the Commission no thereto, must be filed through the longer accepts any hand or messenger electronic comment filing system SUMMARY: In this document, the Federal delivered filings. This is a temporary available for that proceeding, and must Communications Commission measure taken to help protect the health be filed in their native format (e.g., .doc, (Commission) seeks comment on and safety of individuals, and to .xml, .ppt, searchable .pdf). -
Secretariat Distr.: General 11 October 2006
United Nations ST/SG/SER.E/489 Secretariat Distr.: General 11 October 2006 Original: English Committee on the Peaceful Uses of Outer Space Information furnished in conformity with the Convention on Registration of Objects Launched into Outer Space Note verbale dated 16 March 2006 from the Permanent Mission of Canada to the United Nations (Vienna) addressed to the Secretary-General The Permanent Mission of Canada to the United Nations (Vienna) presents its compliments to the Secretary-General of the United Nations and, in accordance with article IV of the Convention on Registration of Objects Launched into Outer Space (General Assembly resolution 3235 (XXIX), annex), has the honour to transmit launch information and technical data concerning Canadian space objects MSAT-1, Nimiq-1, Anik F-1, Canadarm-2, MBS, Nimiq-2, MOST, CanX-1, SciSat and Anik F-2 (see annex). V.06-57629 (E) 271006 271006 *0657629* ST/SG/SER.E/489 Annex Registration data for Canadian space objects* 1. MSAT-1 Names of Launching States: Canada France Designator: MSAT-1 Date and territory or location 20 April 1996 of launch: Kourou, French Guiana Launch vehicle: Ariane 4 Orbital parameters Nodal period: Geostationary Earth orbit Inclination: Controlled to zero ± 0.05 degrees Apogee: Kept between 15 kilometres and 30 kilometres above the synchronous radius Perigee: Kept between 15 kilometres and 30 kilometres below the synchronous radius Longitude: 106.5 degrees West Frequencies and transmitter power: Uplink: 1631.5-1660.5 MHz Downlink: 1530-1559 MHz Uplink: 13.0-13.15 GHz and 13.2-13.25 GHz Downlink: 10.75-10.95 GHz Purpose: Mobile communications—voice and data Operating entity: Mobile Satellite Ventures (Canada) Inc. -
Design of Power, Propulsion, and Thermal Sub-Systems for a 3U Cubesat Measuring Earth’S Radiation Imbalance
Article Design of Power, Propulsion, and Thermal Sub-Systems for a 3U CubeSat Measuring Earth’s Radiation Imbalance Jack Claricoats 1,† and Sam M. Dakka 2,*,† 1 Department of Engineering and Math, Sheffield Hallam University, Howard Street, Sheffield S1 1WB, UK; [email protected] 2 Department of Mechanical, Materials and Manufacturing Engineering, The University of Nottingham, University Park, Nottingham NG7 2RD, UK * Correspondence: [email protected]; Tel.: +44-115-748-6853 † These authors contributed equally to this work. Received: 22 April 2018; Accepted: 6 June 2018; Published: 11 June 2018 Abstract: The paper presents the development of the power, propulsion, and thermal systems for a 3U CubeSat orbiting Earth at a radius of 600 km measuring the radiation imbalance using the RAVAN (Radiometer Assessment using Vertically Aligned NanoTubes) payload developed by NASA (National Aeronautics and Space Administration). The propulsion system was selected as a Mars-Space PPTCUP -Pulsed Plasma Thruster for CubeSat Propulsion, micro-pulsed plasma thruster with satisfactory capability to provide enough impulse to overcome the generated force due to drag to maintain an altitude of 600 km and bring the CubeSat down to a graveyard orbit of 513 km. Thermal analysis for hot case found that the integration of a black high-emissivity paint and MLI was required to prevent excessive heating within the structure. Furthermore, the power system analysis successfully defined electrical consumption scenarios for the CubeSat’s 600 km orbit. The analysis concluded that a singular 7 W solar panel mounted on a sun-facing side of the CubeSat using a sun sensor could satisfactorily power the electrical system throughout the hot phase and charge the craft’s battery enough to ensure constant electrical operation during the cold phase, even with the additional integration of an active thermal heater. -
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.