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The Early Explorers by Andrew J
The Early Explorers by Andrew J. LePage August 8, 1999 Among these programs were the next generation of Introduction Explorer satellites the ABMA was planning. In the chaos that swept the United States after the launching of the first Soviet Sputniks, a variety of The First New Explorers satellite programs was sponsored by the Department The first of the new series of larger Explorer satellites of Defense (DoD) to supplement (and in some cases was the 39.7 kilogram (87.5 pound) satellite NASA supplant) the country's flagging "official" satellite designated as S-1. Built by JPL, the spin stabilized program, Vanguard. One of the stronger programs S-1 consisted of a pair of fiberglass cones joined at was sponsored by the ABMA (Army Ballistic Missile their bases with a diameter and height of 76 Agency) with its engineering team lead by the centimeters each. The scientific payload consisted of German rocket expert, Wernher von Braun. Using instruments to study cosmic rays, solar X-ray and the Juno I launch vehicle, the ABMA team launched ultraviolet emissions, micrometeorites, as well as the America's first satellite, Explorer 1, which was built globe's heat balance. This was all powered by a bank by Caltech's Jet Propulsion Laboratory (JPL) (see of 15 nickel-cadmium batteries recharged by 3,000 Explorer: America's First Satellite in the February solar cells mounted on the satellite's exterior. This 1998 issue of SpaceViews). advanced payload was equipped with a timer to turn itself off after a year in orbit. While these first satellites returned a wealth of new data, they were limited by the tiny 11 kilogram (25 Explorer S-1 was launched from Cape Canaveral on pound) payload capability of the Juno I. -
Windows 7 Operating Guide
Welcome to Windows 7 1 1 You told us what you wanted. We listened. This Windows® 7 Product Guide highlights the new and improved features that will help deliver the one thing you said you wanted the most: Your PC, simplified. 3 3 Contents INTRODUCTION TO WINDOWS 7 6 DESIGNING WINDOWS 7 8 Market Trends that Inspired Windows 7 9 WINDOWS 7 EDITIONS 10 Windows 7 Starter 11 Windows 7 Home Basic 11 Windows 7 Home Premium 12 Windows 7 Professional 12 Windows 7 Enterprise / Windows 7 Ultimate 13 Windows Anytime Upgrade 14 Microsoft Desktop Optimization Pack 14 Windows 7 Editions Comparison 15 GETTING STARTED WITH WINDOWS 7 16 Upgrading a PC to Windows 7 16 WHAT’S NEW IN WINDOWS 7 20 Top Features for You 20 Top Features for IT Professionals 22 Application and Device Compatibility 23 WINDOWS 7 FOR YOU 24 WINDOWS 7 FOR YOU: SIMPLIFIES EVERYDAY TASKS 28 Simple to Navigate 28 Easier to Find Things 35 Easy to Browse the Web 38 Easy to Connect PCs and Manage Devices 41 Easy to Communicate and Share 47 WINDOWS 7 FOR YOU: WORKS THE WAY YOU WANT 50 Speed, Reliability, and Responsiveness 50 More Secure 55 Compatible with You 62 Better Troubleshooting and Problem Solving 66 WINDOWS 7 FOR YOU: MAKES NEW THINGS POSSIBLE 70 Media the Way You Want It 70 Work Anywhere 81 New Ways to Engage 84 INTRODUCTION TO WINDOWS 7 6 WINDOWS 7 FOR IT PROFESSIONALS 88 DESIGNING WINDOWS 7 8 WINDOWS 7 FOR IT PROFESSIONALS: Market Trends that Inspired Windows 7 9 MAKE PEOPLE PRODUCTIVE ANYWHERE 92 WINDOWS 7 EDITIONS 10 Remove Barriers to Information 92 Windows 7 Starter 11 Access -
Information Summaries
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 -
Novell® Platespin® Recon 3.7.4 User Guide 5.6.4 Printing and Exporting Reports
www.novell.com/documentation User Guide Novell® PlateSpin® Recon 3.7.4 September 2012 Legal Notices Novell, Inc., makes no representations or warranties with respect to the contents or use of this documentation, and specifically disclaims any express or implied warranties of merchantability or fitness for any particular purpose. Further, Novell, Inc., reserves the right to revise this publication and to make changes to its content, at any time, without obligation to notify any person or entity of such revisions or changes. Further, Novell, Inc., makes no representations or warranties with respect to any software, and specifically disclaims any express or implied warranties of merchantability or fitness for any particular purpose. Further, Novell, Inc., reserves the right to make changes to any and all parts of Novell software, at any time, without any obligation to notify any person or entity of such changes. Any products or technical information provided under this Agreement may be subject to U.S. export controls and the trade laws of other countries. You agree to comply with all export control regulations and to obtain any required licenses or classification to export, re-export or import deliverables. You agree not to export or re-export to entities on the current U.S. export exclusion lists or to any embargoed or terrorist countries as specified in the U.S. export laws. You agree to not use deliverables for prohibited nuclear, missile, or chemical biological weaponry end uses. See the Novell International Trade Services Web page (http://www.novell.com/info/exports/) for more information on exporting Novell software. -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Abundances 164 ACE (Advanced Composition Explorer) 1, 21, 60, 71
Index abundances 164 CIR (corotating interaction region) 3, ACE (Advanced Composition Explorer) 1, 14À15, 32, 36À37, 47, 62, 108, 151, 21, 60, 71, 170À171, 173, 175, 177, 254À255 200, 251 energetic particles 63, 154 SWICS 43, 86 Climax neutron monitor 197 ACRs (anomalous cosmic rays) 10, 12, 197, CME (coronal mass ejection) 3, 14À15, 56, 258À259 64, 86, 93, 95, 123, 256, 268 CIRs 159 composition 268 pickup ions 197 open flux 138 termination shock 197, 211 comets 2À4, 11 active longitude 25 ComptonÀGetting effect 156 active region 25 convection equation tilt 25 diffusion 204 activity cycle (see also solar cycle) 1À2, corona 1À2 11À12 streamers 48, 63, 105, 254 Advanced Composition Explorer see ACE temperature 42 Alfve´n waves 116, 140, 266 coronal hole 30, 42, 104, 254, 265 AMPTE (Active Magnetospheric Particle PCH (polar coronal hole) 104, 126, 128 Tracer Explorer) mission 43, 197, coronal mass ejections see CME 259 corotating interaction regions see CIR anisotropy telescopes (AT) 158 corotating rarefaction region see CRR Cosmic Ray and Solar Particle Bastille Day see flares Investigation (COSPIN) 152 bow shock 10 cosmic ray nuclear composition (CRNC) butterfly diagram 24À25 172 cosmic rays 2, 16, 22, 29, 34, 37, 195, 259 Cassini mission 181 anomalous 195 CELIAS see SOHO charge state 217 CH see coronal hole composition 196, 217 CHEM 43 convection–diffusion model 213 282 Index cosmic rays (cont.) Energetic Particle Composition Experiment drift 101, 225 (EPAC) 152 force-free approximation 213 energetic particle 268 galactic 195 anisotropy 156, -
Nowak 2019 Apj 874 69
Downloaded from orbit.dtu.dk on: Oct 05, 2021 Chandra-HETGS Characterization of an Outflowing Wind in the Accreting Millisecond Pulsar IGR J17591–2342 Nowak, Michael A.; Paizis, Adamantia; Jaisawal, Gaurava Kumar; Chenevez, Jerome; Chaty, Sylvain; Fortin, Francis; Rodriguez, Jerome; Wilms, Jorn Published in: Astrophysical Journal Link to article, DOI: 10.3847/1538-4357/ab0a71 Publication date: 2019 Document Version Publisher's PDF, also known as Version of record Link back to DTU Orbit Citation (APA): Nowak, M. A., Paizis, A., Jaisawal, G. K., Chenevez, J., Chaty, S., Fortin, F., Rodriguez, J., & Wilms, J. (2019). Chandra-HETGS Characterization of an Outflowing Wind in the Accreting Millisecond Pulsar IGR J17591–2342. Astrophysical Journal, 874(1), [69]. https://doi.org/10.3847/1538-4357/ab0a71 General rights Copyright and moral rights for the publications made accessible in the public portal are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal requirements associated with these rights. Users may download and print one copy of any publication from the public portal for the purpose of private study or research. You may not further distribute the material or use it for any profit-making activity or commercial gain You may freely distribute the URL identifying the publication in the public portal If you believe that this document breaches copyright please contact us providing details, and we will remove access to the work immediately and investigate your claim. The Astrophysical Journal, 874:69 (13pp), 2019 March 20 https://doi.org/10.3847/1538-4357/ab0a71 © 2019. -
<> CRONOLOGIA DE LOS SATÉLITES ARTIFICIALES DE LA
1 SATELITES ARTIFICIALES. Capítulo 5º Subcap. 10 <> CRONOLOGIA DE LOS SATÉLITES ARTIFICIALES DE LA TIERRA. Esta es una relación cronológica de todos los lanzamientos de satélites artificiales de nuestro planeta, con independencia de su éxito o fracaso, tanto en el disparo como en órbita. Significa pues que muchos de ellos no han alcanzado el espacio y fueron destruidos. Se señala en primer lugar (a la izquierda) su nombre, seguido de la fecha del lanzamiento, el país al que pertenece el satélite (que puede ser otro distinto al que lo lanza) y el tipo de satélite; este último aspecto podría no corresponderse en exactitud dado que algunos son de finalidad múltiple. En los lanzamientos múltiples, cada satélite figura separado (salvo en los casos de fracaso, en que no llegan a separarse) pero naturalmente en la misma fecha y juntos. NO ESTÁN incluidos los llevados en vuelos tripulados, si bien se citan en el programa de satélites correspondiente y en el capítulo de “Cronología general de lanzamientos”. .SATÉLITE Fecha País Tipo SPUTNIK F1 15.05.1957 URSS Experimental o tecnológico SPUTNIK F2 21.08.1957 URSS Experimental o tecnológico SPUTNIK 01 04.10.1957 URSS Experimental o tecnológico SPUTNIK 02 03.11.1957 URSS Científico VANGUARD-1A 06.12.1957 USA Experimental o tecnológico EXPLORER 01 31.01.1958 USA Científico VANGUARD-1B 05.02.1958 USA Experimental o tecnológico EXPLORER 02 05.03.1958 USA Científico VANGUARD-1 17.03.1958 USA Experimental o tecnológico EXPLORER 03 26.03.1958 USA Científico SPUTNIK D1 27.04.1958 URSS Geodésico VANGUARD-2A -
2011–2012 Catalog Ii Capitol College 2011-2012 Catalog
2011–2012 catalog ii Capitol College 2011-2012 Catalog General Information General Information . 1 Locations . 4 Mission and Philosophy . 4 History . 6 Centers of Excellence . 7 Affiliations, Memberships and Partnerships . 8 Online Learning . 10 Academic Policies Academic Policies and Procedures . 11 Scholastic Standing . 13 Academic Performance . 15 Matriculation . 16 Transfer Credits . 18 Tuition/Financial Aid Tuition and Fees . 21 Payment Options . 22 Financial Aid . 24 Undergraduate Studies Undergraduate Program Offerings . 30 Undergraduate Admissions . 30 Astronautical Engineering . 35 Business Administration . 36 Computer Engineering . 37 Computer Engineering Technology . 38 Computer Science . 40 Electrical Engineering . 41 Electronics Engineering Technology . 42 Information Assurance . 44 Management of Information Technology . 45 Software Engineering . 46 Software and Internet Applications . 47 Telecommunications Engineering Technology . 48 Certificates . 50 Graduate Studies Graduate Program Offerings . 53 Doctorate Admissions . 53 Master’s Admissions . 54 Information Assurance (DSc) . 56 Business Administration (MBA) . 57 2011-2012 Catalog iii Astronautical Engineering . 58 Computer Science . 59 Electrical Engineering . 60 Information Assurance (MS) . 61 Information and Telecommunications Systems Management . 62 Internet Engineering . 63 Post-baccalaureate Certificates . 64 Non Credit Course and Certificate Offerings . 66 Courses Course Descriptions . 67 Resources Board of Trustees . 100 Advisory Boards . 101 Administration . 103 Faculty . 106 Calendar . 110 Index . 122 Map and Directions . 124 iv Capitol College The following offices are open as General Information indicated (EST) . Directory Admissions M, F 9 a.m.- 5 p.m. Capitol College T-Th 9 a .m .- 7 p .m . 11301 Springfield Road Saturday appointments are available. Laurel, MD 20708-9758 Business Office Main Telephone Numbers M, F 9 a.m.- 5 p.m. Information General 301-369-2800 T-Th 9 a .m .- 7 p .m . -
2010–2011 Catalog
2010–2011 catalog 2010-2011 Catalog General Information General Information . 1 Locations . 4 Mission and Philosophy . 4 History . 6 Partnerships . 7 Online Learning . 10 Academic Policies Academic Policies and Procedures . 11 Scholastic Standing . 13 Academic Performance . 15 Matriculation . 16 Transfer Credits . 18 Tuition/Financial Aid Tuition and Fees . 21 Financial Aid . 24 Undergraduate Studies Undergraduate Program Offerings . 30 Undergraduate Admissions . 30 Astronautical Engineering . 35 Business Administration . 36 Computer Engineering . 37 Computer Engineering Technology . 38 Computer Science . 40 Electrical Engineering . 41 Electronics Engineering Technology . 42 Information Assurance . 44 Management of Information Technology . 45 Software Engineering . 46 Software and Internet Applications . 47 Telecommunications Engineering Technology . 48 Certificates . 50 Non-degree Certification Programs . 53 Graduate Studies Graduate Program Offerings . 54 Graduate Admissions . 54 Information Assurance (DSc) . 56 Business Administration . 57 Computer Science . 58 Electrical Engineering . 59 2010-2011 Catalog iii Information Assurance (MS) . 60 Information and Telecommunications Systems Management . 61 Internet Engineering . 62 Post-baccalaureate Certificates . 63 Courses Course Descriptions . 65 Resources Board of Trustees . 100 Advisory Boards . 101 Administration . 103 Faculty . 106 Calendar . 110 Index . 122 Map and Directions . 124 iv Capitol College The following offices are open as General Information indicated (EST) . Directory Admissions M, F 9 a .m .- 5 p .m . Capitol College T-Th 9 a .m .- 7 p .m . 11301 Springfield Road Saturday appointments are available . Laurel, MD 20708-9758 Business Office Main Telephone Numbers M, F 9 a .m .- 5 p .m . General Information 301-369-2800 T-Th 9 a .m .- 7 p .m . 888-522-7486 Financial Aid Admissions M, F 9 a .m .-5 p .m . -
An Eco Explorer Is a Person Who Investigates
Eco Explorer n eco explorer is a person who investigates A environmental issues and works to make positive changes to the environment. In this badge, you’ll be an eco explorer as you take a look at different environmental issues and choose one to explore further. Steps 1. Meet an eco explorer 2. Explore biodiversity 3. Investigate a global ecosystem issue 4. Plan a trip to explore and work on an issue 5. Share what you learned Purpose When I’ve earned this badge, I’ll have researched different environmental issues and taken at least one trip to see how an area is impacted. Prepare Ahead: Before you start this badge, learn the Leave No Trace Seven Principles so you can follow them as you work through the steps. You can read about them on page three. ECO EXPLORER 1 Every step has three choices. Do ONE choice to complete each step. Inspired? STEP Meet an Do more! 1 eco explorer With help from an adult, arrange to talk to an eco explorer about their work, or research one in books or online. An eco explorer can be anyone who has taken their passion for the environment and used it to make a difference. What inspired them to get involved with environmental issues? How have they impacted the world? CHOICES—DO ONE: Talk to a traveler who has taken a trip to explore an environmental issue or who is interested in eco-friendly travel. (You might get inspired by reading about the conservation-themed Girl Scout Destination trips at www.girlscouts.org/destinations.) How can people travel in an environmentally-friendly way? How can travel be used to make a difference in the world? If you have a trip planned in the future, you might talk about it and ask for tips on making it more eco-friendly. -
Magnetic Cleanliness Program on Cubesats and Nanosatellites For
JOURNAL OF AERONAUTICS AND SPACE TECHNOLOGIES (ISSN : 1304-0448) January 2020 Volume 13 Number 1 www.jast.hho.edu.tr Research Article Magnetic Cleanliness Program on CubeSats and Nanosatellites for Improved Attitude Stability Abdelmadjid LASSAKEUR 1 , Craig UNDERWOOD 2 , Benjamin TAYLOR 2 , Richard DUKE2 1 Satellite Development Center, Algerian Space Agency, BP 4065, Ibn Rochd USTO, 31130 Oran, Algeria, [email protected], https://orcid.org/0000-0002-4538-6985 2 Surrey Space Centre, University of Surrey, Guildford GU2 7XH, United Kingdom, [email protected], [email protected], [email protected], https://orcid.org/0000-0002-7001-5510, https://orcid.org/0000-0003-3635-003X, https://orcid.org/0000-0003-4450- 7981 Article Info Abstract CubeSats are being increasingly specified and utilized for demanding astronomical and Earth observation missions where precise pointing and stability are critical requirements. Such precision is difficult to achieve in the case of CubeSats, mainly because of their small moment of inertia, this means that even small disturbance torques, such as those due to a residual magnetic moment are an issue and have a significant effect on the attitude of nanosatellites, when a high degree of stability is required. Also, hardware limitations in terms of power, weight and size make the task more challenging. Recently, a PhD research program has been undertaken at the University of Surrey to investigate the Received: July 18, 2019 magnetic characteristics of CubeSats. It has been found that the disturbances may Accepted: November 22, 2019 be mitigated by good engineering practice, in terms of reducing the use of Online: January 23, 2020 permeable materials and minimizing current-loop area.