OFEK-9 Soars Into Space
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Strategic Assessment, Vol 16, No 1
Volume 16 | No. 1 | April 2013 Leading from Behind: The “Obama Doctrine” and US Policy in the Middle East | Sanford Lakoff Eleven Years to the Arab Peace Initiative: Time for an Israeli Regional Strategy | Ilai Alon and Gilead Sher The Emergence of the Sunni Axis in the Middle East | Yoel Guzansky and Gallia Lindenstrauss Islam and Democracy: Can the Two Walk Together? | Yoav Rosenberg The US and Israel on Iran: Whither the (Dis)Agreement? | Ephraim Kam Walking a Fine Line: Israel, India, and Iran | Yiftah S. Shapir Response Essays Civilian Casualties of a Military Strike in Iran | Ephraim Asculai If it Comes to Force: A Credible Cost-Benefit Analysis of the Military Option against Iran | Amos Yadlin, Emily B. Landau, and Avner Golov המכון למחקרי ביטחון לאומי THE INSTITUTE FOR NATIONAL SECURcITY STUDIES INCORPORATING THE JAFFEE bd CENTER FOR STRATEGIC STUDIES Strategic ASSESSMENT Volume 16 | No. 1 | April 2013 CONTENTS Abstracts | 3 Leading from Behind: The “Obama Doctrine” and US Policy in the Middle East | 7 Sanford Lakoff Eleven Years to the Arab Peace Initiative: Time for an Israeli Regional Strategy | 21 Ilai Alon and Gilead Sher The Emergence of the Sunni Axis in the Middle East | 37 Yoel Guzansky and Gallia Lindenstrauss Islam and Democracy: Can the Two Walk Together? | 49 Yoav Rosenberg The US and Israel on Iran: Whither the (Dis)Agreement? | 61 Ephraim Kam Walking a Fine Line: Israel, India, and Iran | 75 Yiftah S. Shapir Response Essays Civilian Casualties of a Military Strike in Iran | 87 Ephraim Asculai If it Comes to Force: A Credible Cost-Benefit Analysis of the Military Option against Iran | 95 Amos Yadlin, Emily B. -
Rafael Space Propulsion
Rafael Space Propulsion CATALOGUE A B C D E F G Proprietary Notice This document includes data proprietary to Rafael Ltd. and shall not be duplicated, used, or disclosed, in whole or in part, for any purpose without written authorization from Rafael Ltd. Rafael Space Propulsion INTRODUCTION AND OVERVIEW PART A: HERITAGE PART B: SATELLITE PROPULSION SYSTEMS PART C: PROPELLANT TANKS PART D: PROPULSION THRUSTERS Satellites Launchers PART E: PROPULSION SYSTEM VALVES PART F: SPACE PRODUCTION CAPABILITIES PART G: QUALITY MANAGEMENT CATALOGUE – Version 2 | 2019 Heritage PART A Heritage 0 Heritage PART A Rafael Introduction and Overview Rafael Advanced Defense Systems Ltd. designs, develops, manufactures and supplies a wide range of high-tech systems for air, land, sea and space applications. Rafael was established as part of the Ministry of Defense more than 70 years ago and was incorporated in 2002. Currently, 7% of its sales are re-invested in R&D. Rafael’s know-how is embedded in almost every operational Israel Defense Forces (IDF) system; the company has a special relationship with the IDF. Rafael has formed partnerships with companies with leading aerospace and defense companies worldwide to develop applications based on its proprietary technologies. Offset activities and industrial co-operations have been set-up with more than 20 countries world-wide. Over the last decade, international business activities have been steadily expanding across the globe, with Rafael acting as either prime-contractor or subcontractor, capitalizing on its strengths at both system and sub-system levels. Rafael’s highly skilled and dedicated workforce tackles complex projects, from initial development phases, through prototype, production and acceptance tests. -
Satellite Characterization, Classification, and Operational Assessment Via the Exploitation of Remote Photoacoustic Signatures
Satellite Characterization, Classification, and Operational Assessment Via the Exploitation of Remote Photoacoustic Signatures Justin Spurbeck1 The University of Texas at Austin Moriba K. Jah, Ph.D.2 The University of Texas at Austin Daniel Kucharski, Ph.D.3 Space Environment Research Centre & The University of Texas at Austin James C. S. Bennett, Ph.D.4 EOS Space Systems & Space Environment Research Centre James G. Webb, Ph.D.5 EOS Space Systems ABSTRACT Current active satellite maneuver detection techniques have the ability to detect maneuvers as quickly as fifteen minutes post maneuver for large delta-v when using angles only optical tracking. Medium to small magnitude burn detection times range from 6-24 hours or more. Small magnitude burns may be indistinguishable from natural perturbative effects if passive techniques are employed. Utilizing a photoacoustic signature detection scheme would allow for near real time maneuver detection and spacecraft parameter estimation. We define the acquisition of high rate photometry data as photoacoustic sensing because the data can be played back as an acoustic signal. Studying the operational frequency spectra, profile, and aural perception of an active satellite event such as a thruster fire or any on-board component activation will provide unique signature identifiers that support Resident Space Object (RSO) characterization efforts. A thruster fire induces vibrations in a satellite body which then modulate incident rays of light. If the reflected photon flux is sampled at a sufficient rate, the change in light intensity due to the propulsive event can be detected. Sensing vibrational mode changes allows for a direct timestamp of thruster fire events and thus makes possible the near real time estimation of spacecraft delta-v and maneuver type if coupled with active observations immediately post maneuver. -
Synthetic Aperture Radar
Synthetic Aperture Radar Subjects: Information Technology & Data Management Submitted by: Sung Wook Paek Definition SAR constellations Table of Contents [Hide] 1. Introduction Space-based radar observation has growing potentials for monitoring the global biospheric diversity subject to anthropogenic drivers at geological scales [1]. The performance of radar is less affected by weather and sunlight conditions than that of optical sensors. Satellites with onboard sensors can provide comprehensive coverage of remote areas or vast regions that may be too costly for unmanned aerial vehicles (UAVs) or ground-based platforms, provided that all platforms provide congruent results via calibrations [2][3][4]. Therefore, it was Seasat, the first satellite dedicated to remote sensing of the Earth’s oceans, that carried the first synthetic aperture radar (SAR) and other radar instruments operable in space. Despite these advantages, miniaturization of radar-carrying satellites was rather slow compared to satellites carrying optical devices due to the lack of commercial-off-the-shelf (COTS) components as well as challenging design requirements for the satellite platform [5][6]. Representative use cases of space-based radar include altimetry, sounding, scatterometry, and so forth in the studies of land, cryosphere, and oceans. Biospheric monitoring is another useful application because radar has high sensitivity in detecting surface changes in a target area and discriminating mobile targets against a background [7]. This paper will consider mainly SAR because of its three-dimensional mapping capability through interferometry. The heritage of Seasat has influenced many of later SAR missions for decades, as listed in Table 1 [8][9][10][11][12][13]; for instance, Shuttle Image Radar (SIR) missions used spare parts of the previous Seasat mission onboard Space Shuttles to test SAR image applications in land use, geology, hydrology, and forestry [14][15]. -
High Altitude Nuclear Detonations (HAND) Against Low Earth Orbit Satellites ("HALEOS")
High Altitude Nuclear Detonations (HAND) Against Low Earth Orbit Satellites ("HALEOS") DTRA Advanced Systems and Concepts Office April 2001 1 3/23/01 SPONSOR: Defense Threat Reduction Agency - Dr. Jay Davis, Director Advanced Systems and Concepts Office - Dr. Randall S. Murch, Director BACKGROUND: The Defense Threat Reduction Agency (DTRA) was founded in 1998 to integrate and focus the capabilities of the Department of Defense (DoD) that address the weapons of mass destruction (WMD) threat. To assist the Agency in its primary mission, the Advanced Systems and Concepts Office (ASCO) develops and maintains and evolving analytical vision of necessary and sufficient capabilities to protect United States and Allied forces and citizens from WMD attack. ASCO is also charged by DoD and by the U.S. Government generally to identify gaps in these capabilities and initiate programs to fill them. It also provides support to the Threat Reduction Advisory Committee (TRAC), and its Panels, with timely, high quality research. SUPERVISING PROJECT OFFICER: Dr. John Parmentola, Chief, Advanced Operations and Systems Division, ASCO, DTRA, (703)-767-5705. The publication of this document does not indicate endorsement by the Department of Defense, nor should the contents be construed as reflecting the official position of the sponsoring agency. 1 Study Participants • DTRA/AS • RAND – John Parmentola – Peter Wilson – Thomas Killion – Roger Molander – William Durch – David Mussington – Terry Heuring – Richard Mesic – James Bonomo • DTRA/TD – Lewis Cohn • Logicon RDA – Les Palkuti – Glenn Kweder – Thomas Kennedy – Rob Mahoney – Kenneth Schwartz – Al Costantine – Balram Prasad • Mission Research Corp. – William White 2 3/23/01 2 Focus of This Briefing • Vulnerability of commercial and government-owned, unclassified satellite constellations in low earth orbit (LEO) to the effects of a high-altitude nuclear explosion. -
USGS Earth Resources Observation and Science (EROS) Center
USGS Earth Resources Observation and Science (EROS) Center National Satellite Land Remote Sensing Data Archive Report June 2019 U.S. Department of the Interior U.S. Geological Survey NATIONAL SATELLITE LAND REMOTE SENSING DATA ARCHIVE REPORT June 2019 Questions or comments concerning data holdings referenced in this report may be directed to: John Faundeen Archivist U.S. Geological Survey EROS Center 47914 252nd Street Sioux Falls, SD 57198 USA Tel: (605) 594-6092 E-mail: [email protected] NATIONAL SATELLITE LAND REMOTE SENSING DATA ARCHIVE REPORT June 2019 FILM SOURCE Date Range Frames Declassification I CORONA (KH-1, KH-2, KH-3, KH-4, KH-4A, KH-4B) Jul-60 May-72 907,788 ARGON (KH-5) May-62 Aug-64 36,887 LANYARD (KH-6) Jul-60 Aug-63 908 Total Declass I 945,583 Declassification II KH-7 Jul-63 Jun-67 17,814 KH-9 Mar-73 Oct-80 29,140 Total Declass II 46,954 Declassification III HEXAGON (KH-9) Jun-71 Oct-84 40,638 Total Declass III 40,638 Large Format Camera Large Format Camera Oct-84 Oct-84 2,139 Total Large Format Camera 2,139 Landsat MSS Landsat MSS 70-mm Jul-72 Sep-78 1,342,187 Landsat MSS 9-inch Mar-78 Oct-92 1,338,195 Total Landsat MSS 2,680,382 Landsat TM Landsat TM 9-inch Aug-82 May-88 175,665 Total Landsat TM 175,665 Landsat RBV Landsat RBV 70-mm Jul-72 Mar-83 138,168 Total Landsat RBV 138,168 Gemini Gemini Jun-65 Nov-66 2,447 Total Gemini 2,447 Skylab Skylab May-73 Feb-74 50,486 Total Skylab 50,486 TOTAL FILM SOURCE 4,082,462 NATIONAL SATELLITE LAND REMOTE SENSING DATA ARCHIVE REPORT June 2019 DIGITAL SOURCE Scenes Total Size (bytes) -
Radar Ortho Suite
Technical Specifications Radar Ortho Suite The Radar Ortho Suite includes rigorous and rational function models developed to compensate for distortions and produce orthorectified radar images. Distortions caused by the platform (position, velocity, and orientation), the sensor (orientation, integration time, and field of view) the Earth (geoid, ellipsoid, and relief), and the projection (ellipsoid and cartographic) are all taken into account using these models. The models reflect the physical reality of the complete viewing geometry and correct all distortions generated during the image formation. Module Prerequisites The Radar Ortho Suite is an add-on to Geomatica. It requires Geomatica Core or Geomatica Prime as a pre-requisite. Supported Radar Formats The Radar Ortho Suite supports the following radar sensors. • ASAR o ASAR 1B format • COSMO-SkyMed o Level 0 (RAW) o Level 1A (SCS) o Level 1B (DGM) • ERS 1/2(CEOS) o ERS CD provides different levels of processing. We recommend the georeferenced level for images produced in Canada and the PRI level produced by ESA. • Gaofen-3 (GF3) o Level 1A SLC data with an associated RPC model for the following observation modes: . Spotlight [SL] . Ultra-fine stripmap [UFS] . Fine stripmap [FSI] . Wide fine stripmap [FSII] . Quad-pol stripmap [QPSI] . Wide quad-pol stripmap [QPSII] . Wave [WAV] • Huanjing (HJ-1C) o 1C Level 2 format • JERS1 (LGSOWG) o JERS-1 CD provides different levels of processing. We recommend that you use a georeferenced level or equivalent for highest accuracy. OrthoEngine only works for descending order images. • KOMPSAT-5 o L1A SCS_U: Single Look Complex Slant Un-balanced o L1A SCS_B: Single Look Complex Slant Balanced o L1B DSM_U: Detected, Slant Range, Multilook Un-equalized o L1B DSM_U: Detected, Slant Range, Multilook o L1B DGM_B: Detected, Ground projected, Multilook Balanced The information in this document is subject to change without notice and should not be construed as a commitment by PCI Geomatics. -
Technical Profile 4
Technical Profile 4 General Specifications • Orbital location 65° East Scheduled for launch in 2013, Spacecom’s AMOS-4 satellite will establish a new orbital position at 65°E, providing a full range of • Frequency band Ku, Ka satellite services for India, Southeast Asia, Russia, the Middle East • Number of available and other additional service areas. Ku-band Transponders 8 x 108MHz • Number of available AMOS-4's multiple Ku and Ka transponders create a powerful platform, Ka-band Transponders 4 x 216MHz enabling a wide range of cross-band, cross-beam connectivity options. For our customers, this means extensive broadcast and broadband • Service areas reach into the vast urban and rural areas of these regions. Available - Ku-band beams: satellite services for customers include Direct-To-Home (DTH), video two shaped steerable beams covering Russia distribution, VSAT communications and broadband Internet. and India with optional steering to: Southeast Asia, the Middle East, Central Asia, India, South Africa and Central East Europe With its new orbital slot, additional capacity, expanded coverage areas and cross-region connectivity, AMOS-4 positions Spacecom at the - Ka-band beam: one shaped steerable beam covering the Middle forefront of international satellite operators delivering comprehensive East. Optional steering to: Russia, India, China, satellite solutions. Our constellation, which provides comprehensive Central Asia, Southeast Asia, and South Africa coverage for Europe, Africa and the Middle East, also includes our AMOS-2 and AMOS-3 satellites, co-located at the 4°W orbital "Hot • Full cross beam connectivity Ku to Ku Spot”, and AMOS-5 located at 17°E. • Full cross band connectivity Ka to Ku – U/L in Ka beam and D/L in any Ku beam • Expected Launch date .............................................2013 space to expand 44 47 49 51 53 India Beam (Ku-1) Parameters Number of Transponders .............. -
AMOS-5 Handnook
AMOS-4 Ku-2 Beam Technical Handbook / Version 1.3 January 2015 This document contains proprietary information of Space-Communication Ltd., and may not be reproduced, copied, disclosed or utilized in any way, in whole or in part, without the prior written consent of Space-Communication Ltd. 1. INTRODUCTION Launched in 2013, Spacecom’s AMOS-4 satellite established a new orbital position at 65°E, providing a full range of satellite services for Asia, Russia, the Middle East as well as other service areas. Picture 1- AMOS-4 Deployed View AMOS-4 Technical Specifications / Space-Communications Ltd. th Gibor Sport Building, 20 fl. 7 Menachem Begin St. Ramat-Gan, 52521, Israel Page 2 of 6 Tel. +972 3 7551000 Fax + 972 3 7551001 email: [email protected] 2. GENERAL SPECIFICATIONS Orbital location..........................................................65° East Launch date...............................................................August 2013 Number of available Ku-band Transponders…………..4 x 108MHz Ku-2 beam coverage……………………………………………....Steerable beam 3. FREQUENCY BANDS AND POLARIZATION Uplink frequencies...................................................... 13.00 to 13.25 GHz 13.75 to 14.00 GHz Vertical/ Horizontal Downlink frequencies................................................. 10.70 to 10.59 MHz 11.20 to 11.45 MHz Vertical/ Horizontal The channels' connectivity is fully flexible. AMOS-4 Technical Specifications / Space-Communications Ltd. th Gibor Sport Building, 20 fl. 7 Menachem Begin St. Ramat-Gan, 52521, Israel Page 3 of 6 Tel. +972 3 7551000 Fax + 972 3 7551001 email: [email protected] 4. PAYLOAD CHARACTERISTICS 4.1. EIRP at Beam Peak Band Ku-2 EIRP [dBW] 91.5 4.2. G/T at Beam Peak Band Ku-2 G/T [dB/K] 3.3 4.3. -
Maximizing the Utility of Satellite Remote Sensing for the Management of Global Challenges
UN-GGIM Exchange Forum Maximizing the Utility of Satellite Remote Sensing for the Management of Global Challenges Paulo Bezerra Managing Director MDA Geospatial Services Inc. paulo@mdacorporation . com RESTRICTION ON USE, PUBLICATION OR DISCLOSURE OF PROPRIETARY INFORMATION This document contains information proprietary to MacDonald, Dettwiler and Associates Ltd., to its subsidiaries, or to a third party to which MacDonald, Dettwiler and Associates Ltd. may have a legal obligation to protect such information from unauthorized disclosure, use or duplication. Any disclosure, use or duplication of this document or of any of the information contained herein for other thanUse, the duplication,specific pur orpose disclosure for which of this it wasdocument disclosed or any is ofexpressly the information prohibited, contained except herein as MacDonald, is subject to theDettwiler restrictions and Assoon thciatese title page Ltd. ofmay this agr document.ee to in writing. 1 MDA Geospatial Services Inc. (GSI) Providing Essential Geospatial Products and Services to a global base of customers. SATELLITE DATA DISTRIBUTION DERIVED INFORMATION SERVICES Copyright © MDA ISI GeoCover Regional Mosaic. Generated Top Image - Copyright © 2002 DigitialGlobe from LANDSAT™ data. Bottom Image - RADARSAT-1 Data © CSA (()2001). Received by the Canada Centre for Remote Sensing. Processed and distributed by MDA Geospatial Services Inc. Use, duplication, or disclosure of this document or any of the information contained herein is subject to the restrictions on the title page of this document. MDA GSI - Satellite Data Distribution Worldwide distributor of radar and optical satellite data RADARSAT-2 GeoEye WorldView RapidEye USA Canada Brazil Chile RADARSAT-2 Data and Products © MACDONALD DETTWILER AND Copyright © 2011 GeoEye ASSOCIATES LTD. -
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 . -
D Ossier De Pres Se
20 Juillet 2017 Venµs (Vegetation and Environment monitoring on a New Microsatellite) PRESSE DE OSSIER D 1 Sommaire INTRODUCTION…………………………………………………. 3 Venus : un satellite remarquable pour trois raisons………3 Un nouvel outil contre le changement climatique………….4 Les objectifs de la mission…………………………................5 Les acteurs de la mission……………………………...............5 L’historique de Venus……………………………………..........6 Un instrument de pointe……………………………………..….7 Une mission innovante……………………………………….....8 Une coopération internationale exemplaire……………..…..9 Un choix de sites géographiques varié………………….…10 Des applications pour des secteurs variés……………..…11 Géographie des 110 sites retenus dans le monde……….12 2 INTRODUCTION Jean-Yves Le Gall, Président du CNES : « Alors que la COP21 et la COP22 ont mis en exergue le rôle fondamental des satellites pour l’étude et la préservation du climat, je me réjouis de voir que les meilleurs ingénieurs du spatial au niveau mondial ont développé ensemble Venµs, qui aidera la communauté internationale à lutter contre le changement climatique et que cette coopération va se poursuivre». Avi Blasberger, Directeur de l'Agence Spatiale Israélienne au Ministère de la Science et de la Technologie : « Venµs est le premier satellite de recherche pour l'environnement conçu par Israël, conjointement avec la France. Il est également le plus grand projet de l'Agence Spatiale Israélienne et nous sommes heureux qu'il ait été créé avec la France. Le lancement du Satellite "Venµs " vient juste avant la célébration des 70 ans des relations étroites d'Israël avec la France, qui seront fêtées l'année prochaine par le biais de différentes activités en France et en Israël. Les capacités de ce satellite démontrent l'innovation et l'audace Israélienne combinée à l’excellence française.