Satellite Constellations - 2021 Industry Survey and Trends
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GT 1020 Datasheet
HARDWARE • DATASHEET GT 1020 Cellular-based telematics for general asset management applications. Complete visibility of transportation and heavy equipment assets, industrial equipment and more. The compact and versatile GT 1020 is designed to fit a wide range of asset tracking 4G LTE cellular applications across various market segments, including transportation, supply communications chain, heavy equipment and maritime. As part of a comprehensive solution that can include cellular connectivity, sensors and a cloud application, the GT 1020 enables remote monitoring of fixed and mobile assets, and delivers actionable data Integrated antennas to ensure complete visibility of operations and enable informed business planning. Feature-rich Quick and easy installation Future proof your solution with global communications over the 4G LTE cellular network with 3G/2G fallback. The GT 1020 features optional Bluetooth support for wireless sensors plus an intelligent reporting system that optimizes power and Compact and rugged airtime usage by adjusting the frequency of location updates based on vehicle motion. An optional CAN Bus interface enables advanced vehicle reporting, analytics and diagnostics, while a backup battery enables reporting for up to 11 Optional CAN Bus support months (depending on reporting frequency) without external power. The device includes a digital input that can be used to report on status changes, such as tire pressure alarms or whether the vehicle is on or off. Feature-rich and versatile Quick and discrete installation Integrated cellular and GPS antennas and mounting options with VHB tape or Long-lasting screws make the GT 1020 quick and easy to install and remove. Its small size backup battery supports covert installations on smaller equipment and assets to deter theft and tampering. -
By Tamman Montanaro
4 Reusable First Stage Rockets y1 = 15.338 m m1 = 2.047 x 10 kg 5 y2 = 5.115 m m2 = 1.613 x 10 kg By Tamman Montanaro What is the moment of inertia? What is the force required from the cold gas thrusters if we assume constancy. Figure 1. Robbert Goddard’s design of the first ever rocket to fly in 1926. Source: George Edward Pendray. The moment of inertia of a solid disk: rper The Rocket Formula Now lets stack a bunch of these solid disk on each other: Length = l Divide by dt Figure 2: Flight path for the Falcon 9; After separation, the first stage orientates itself and prepares itself for landing. Source: SpaceX If we do the same for the hollow cylinder, we get a moment of inertia Launch of: Specific impulse for a rocket: How much mass is lost? What is the mass loss? What is the moment of inertia about the center of mass for these two objects? Divide by m Figure 3: Falcon 9 first stage after landing on drone barge. Source: SpaceX nd On December 22 2015, the Falcon 9 Orbcomm-2 What is the constant force required for its journey halfway (assuming first stage lands successfully. This is the first ever orbital- that the force required to flip it 90o is the equal and opposite to class rocket landing. From the video and flight logs, we Flip Maneuver stabilize the flip). can gather specifications about the first stage. ⃑ How much time does it take for the first stage to descend? We assume this is the time it takes � Flight Specifications for the first stage to reorientate itself. -
November 2020 Worldwide Satellite Magazine
Worldwide Satellite Magazine SatMagazineSatMagazine November 2020 Cover image is couresy of Spacechips. CONNECTING YOU TO THE FUTURE SMALL PACKAGE. 1.35M FIT BIG GAIN. FLEXIBLE INTEGRATED TERMINAL ARSTRAT KA-BAND CERTIFICATION COMPUTER ASSISTED SATCAP MANUAL POINTING OR AUTO-AQUISITION BUILT-IN TUNER & BEACON RECEIVER TRI-BAND X, KU AND WIDEBAND KA FEEDS WITH QUICK CHANGE RF KITS MODULAR & FLEXIBLE MODEM, BUC & LNB OPTIONS SCALABLE: 75CM, 98CM & 1.35M SET-UP BY ONE PERSON IN MINUTES LIGHTWEIGHT IATA-COMPLIANT avltech.comCHECKABLE CASES avltech.com ENABLING YOUR AMBITIONS TO REACH THEIR TARGET Ariane 6 by 2020 Vega C by 2020 Customer-tailored for versatility, reliability, competitiveness. Publishing Operations Senior Columnists This Issue’s Authors Silvano Payne, Publisher + Executive Writer Chris Forrester, Broadgate Publications Rajan Bedi Will Mudge Simon Payne, Chief Technical Officer Karl Fuchs, iDirect Government Services Matteo L. Bemposti Brian O’Toole Hartley G. Lesser, Editorial Director Bob Gough, Goonhilly Earth Station John Dahlia Dr. Anthony Penderis Pattie Lesser, Executive Editor Rebecca M. Cowen-Hirsch, Inmarsat Mark Donaghy Greg Quiggle Donald McGee, Production Manager Ken Peterman, Viasat Joakim Espeland Daniel Smith Andy Bernard, Sales Director Giles Peeters, Track24 Defence Semir Hassanaly James Trevelyan Teresa Sanderson, Operations Director Koen Willems, ST Engineering Newtec John Innes Jean-Claude Tshipama Sean Payne, Business Development Director Dan Makinster, Technical Advisor Features Advertiser Index Advantech Wireless Technologies, Inc. .7 “New Space” Leads a Path on the Ground as well as in Space: . .8 How EO + GSaaS are Driving the Dynamic Ground Segment Transformation . AvL Technologies . .2 by Greg Quiggle, Kratos Arabsat Satellite . .31 European Union to Seek Pan-European Broadand-by-Satellite System? . -
FCC-20-54A1.Pdf
Federal Communications Commission FCC 20-54 Before the Federal Communications Commission Washington, D.C. 20554 In the Matter of ) ) Mitigation of Orbital Debris in the New Space Age ) IB Docket No. 18-313 ) REPORT AND ORDER AND FURTHER NOTICE OF PROPOSED RULEMAKING Adopted: April 23, 2020 Released: April 24, 2020 By the Commission: Chairman Pai and Commissioners O’Rielly, Carr, and Starks issuing separate statements; Commissioner Rosenworcel concurring and issuing a statement. Comment Date: (45 days after date of publication in the Federal Register). Reply Comment Date: (75 days after date of publication in the Federal Register). TABLE OF CONTENTS Heading Paragraph # I. INTRODUCTION .................................................................................................................................. 1 II. BACKGROUND .................................................................................................................................... 3 III. DISCUSSION ...................................................................................................................................... 14 A. Regulatory Approach to Mitigation of Orbital Debris ................................................................... 15 1. FCC Statutory Authority Regarding Orbital Debris ................................................................ 15 2. Relationship with Other U.S. Government Activities ............................................................. 20 3. Economic Considerations ....................................................................................................... -
Ring Road: User Applications on a High Latency Network
User Applications on a High-Latency Network Scott Burleigh 24 January 2014 This research was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration. (c) 2014 California Institute of Technology. Government sponsorship acknowledged. Outline • An infrastructure proposal: a constellation of nanosatellites using delay-tolerant networking to provide low-cost access • An illustration • Some details: capacity, costs • Application latency in this network • Some applications that would work despite the latency • A perspective on using a network • Caveats and outlook 24 January 2014 2 Satellites for Universal Network Access • Earth-orbiting satellites can relay radio communications among sites on Earth. • Can be visible from all points on Earth’s surface, removing geographic and political obstacles. • Not a new idea: – Geostationary (GEO): Exede (ViaSat), HughesNet (EchoStar), WildBlue, StarBand, Intelsat, Inmarsat, Thuraya – Low-Earth Orbiting (LEO): Globalstar, Iridium, Orbcomm, Teledesic 24 January 2014 3 So, Problem Solved? • Maintaining Internet connections with satellites isn’t easy. • GEO satellites do this by ensuring continuous radio contact with ground stations and customer equipment. But: – They are costly, on the order of $300 million (manufacture & launch). – Each one provides communication to a limited part of Earth’s surface. – Each one is a single point of failure. – While data rates are high, round-trip latencies are also high. • LEO constellations do this by constantly switching connections among moving satellites. – Broad coverage areas, low latencies. – But data rates are lower than for GEO, more satellites are needed, and they’re still expensive: $150-$200 million (manufacture and launch). -
Pocketqube Standard Issue 1 7Th of June, 2018
The PocketQube Standard Issue 1 7th of June, 2018 The PocketQube Standard June 7, 2018 Contributors: Organization Name Authors Reviewers TU Delft S. Radu S. Radu TU Delft M.S. Uludag M.S. Uludag TU Delft S. Speretta S. Speretta TU Delft J. Bouwmeester J. Bouwmeester TU Delft - A. Menicucci TU Delft - A. Cervone Alba Orbital A. Dunn A. Dunn Alba Orbital T. Walkinshaw T. Walkinshaw Gauss Srl P.L. Kaled Da Cas P.L. Kaled Da Cas Gauss Srl C. Cappelletti C. Cappelletti Gauss Srl - F. Graziani Important Note(s): The latest version of the PocketQube Standard shall be the official version. 2 The PocketQube Standard June 7, 2018 Contents 1. Introduction ............................................................................................................................................................... 4 1.1 Purpose .............................................................................................................................................................. 4 2. PocketQube Specification ......................................................................................................................................... 4 1.2 General requirements ....................................................................................................................................... 5 2.2 Mechanical Requirements ................................................................................................................................. 5 2.2.1 Exterior dimensions .................................................................................................................................. -
Opportunities for Asia and the Pacific
DIGITAL CONNECTIVITY AND LOW EARTH ORBIT SATELLITE CONSTELLATIONS: OPPORTUNITIES FOR ASIA AND THE PACIFIC John Garrity, Consultant (Digital Connectivity), Digital Technology for Development, [email protected] AN ‘EMERGING CONNECTIVITY INNOVATION’ … 30+ YEARS IN THE MAKING How it started: (1990s) How it ended: (early 2000s) “…in the end the financial, technical and business risks associated with Te l e d e s i c could not be retired.” - Tre n Griffin (Te l e d e s i c employee #4) https://www.wired.com/1997/10/teledesic-mounts-lead-in-new-space-race/ https://25iq.com/2016/07/23/a-dozen-things-i-learned-being-involved-in-one-of-the-most-ambitious- http://personal.ee.surrey.ac.uk/Personal/L.Wood/constellations/teledesic-3d.html startups-ever-conceived-teledesic/ CONTENTS I. BACKGROUND: SATELLITE CONNECTIVITY AS A MEANS FOR BROADBAND INTERNET II. INNOVATION IN LOW EARTH ORBIT SATELLITE CONSTELLATIONS III. IN FOCUS: STARLINK’S DEPLOYMENT, DIFFERENTIATION, AND VIABILITY IV. OPPORTUNITIES AND BARRIERS TO LEVERAGING LOW EARTH ORBIT SATELLITES IN DEVELOPING MEMBER COUNTRIES V. RECOMMENDATIONS: WHAT DEVELOPING MEMBER COUNTRIES CAN DO TO LEVERAGE THE OPPORTUNITY PRESENTED BY LOW EARTH ORBIT SATELLITE CONNECTIVITY FILLS NECESSARY ROLE IN INTERNET ECOSYSTEM Telecommunications Network Infrastructure Elements red lines highlight where satellite is utilized International capacity National backbone (core) Middle-mile (backhaul) Last-mile (access) Regional PoPs Fibre or wireless backhaul Wireless (e.g cellular, Wi-Fi, (microwave, cellular) Fixed wireless access) High-capacity links Base station End User devices (phones, computers, etc.) tower and premises (homes, businesses, etc.) International link (undersea, Wireless (e.g. satellite, Wi-Fi) terrestrial or Fibre-optic satellite) cable landing Satellite backhaul station (GEO, MEO, or LEO) End User devices (phones, computers, etc.) and premises (homes, businesses, etc.) Primary nodes (Points of Presence, PoPs) Fibre or wireless backhaul (microwave, cellular) Wired (e.g. -
Positioning Using IRIDIUM Satellite Signals of Opportunity in Weak Signal Environment
electronics Article Positioning Using IRIDIUM Satellite Signals of Opportunity in Weak Signal Environment Zizhong Tan, Honglei Qin, Li Cong * and Chao Zhao School of Electronic and Information Engineering, Beihang University (BUAA), Beijing 100191, China; [email protected] (Z.T.); [email protected] (H.Q.); [email protected] (C.Z.) * Correspondence: [email protected]; Tel.: +86-1381-0629-638 Received: 9 December 2019; Accepted: 25 December 2019; Published: 27 December 2019 Abstract: In order to get rid of the dependence of the navigation and positioning system on the global navigation satellite system (GNSS), radio, television, satellite, and other signals of opportunity (SOPs) can be used to achieve receiver positioning. The space-based SOPs based on satellites offer better coverage and availability than ground-based SOPs. Based on the related research of Iridium SOPs positioning in the open environment, this paper mainly focuses on the occluded environment and studies the Iridium SOPs positioning technique in weak signal environment. A new quadratic square accumulating instantaneous Doppler estimation algorithm (QSA-IDE) is proposed after analysing the orbit and signal characteristics of the Iridium satellite. The new method can improve the ability of the Iridium weak signal Doppler estimation. The theoretical analysis and positioning results based on real signal data show that the positioning based on Iridium SOPs can be realized in a weak signal environment. The research broadens the applicable environment of the Iridium SOPs positioning, thereby improving the availability and continuity of its positioning. Keywords: signals of opportunity positioning; Iridium; weak signal; instantaneous Doppler 1. Introduction The new methods for receiver positioning based on abundant and various frequency signals have emerged in recent years. -
Orbcomm Announces International Ground
ORBCOMM ANNOUNCES TARGET LAUNCH SCHEDULE FOR SECOND OG2 MISSION SpaceX to conduct static fire of its Falcon 9 rocket next week Rochelle Park, NJ, December 10, 2015 – ORBCOMM Inc. (Nasdaq: ORBC), a global provider of Machine-to-Machine (M2M) and Internet of Things (IoT) solutions, today announced that SpaceX is planning to conduct the static fire of its Falcon 9 rocket on December 16, 2015, which will launch eleven next generation OG2 satellites as part of ORBCOMM’s second and final OG2 Mission at Cape Canaveral Air Force Station, Florida. Once the static fire is completed to verify the readiness of the Falcon 9 rocket, ORBCOMM’s second OG2 Mission is targeted to launch about three days later between 8:00 PM and 9:00 PM ET. ORBCOMM’s OG2 satellites are far more advanced than its current OG1 satellites designed to provide existing customers with significant enhancements, such as faster message delivery, larger message sizes and better coverage at higher latitudes, while drastically increasing network capacity. In addition, the OG2 satellites are equipped with an Automatic Identification System (AIS) payload to receive and report transmissions from AIS-equipped vessels for ship tracking and other maritime navigational and safety efforts, increasing asset visibility and the probability of detection for ORBCOMM’s AIS customers. Please visit our website at http://www.orbcomm.com/og2 for more information and further updates. About ORBCOMM Inc. ORBCOMM Inc. (Nasdaq: ORBC) is a leading global provider of Machine-to-Machine (M2M) communication solutions and the only commercial satellite network dedicated to M2M. ORBCOMM’s unique combination of global satellite, cellular and dual-mode network connectivity, hardware, web reporting applications and software is the M2M industry’s most complete service offering. -
Signature Redacted a U Th O R
A Systems Analysis of CubeSat Constellations with Distributed Sensors by Ayesha Georgina Hein B.S. Astronautical Engineering United States Air Force Academy, 2015 Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY June 2017 @ Massachusetts Institute of Technology 2017. All rights reserved. Signature redacted A u th o r ................................ .--- - -- - - - - - - - - Department of Aeronautics and Astronautics May 25, 2017 Certified by ...................... Signature redacted Y Kerri Cahoy Associate Professor of Aeronautics and Astronautics Thesis Supervisor Accepted by .................. Signature redacted Yodisein . Marzouk ARCHNES Associate Professor of Aeronautics and Astronautics Graduate Program Committee MASSACHUS ITUTE Chair, OF TECHNOLOGY JUL 11 2017 LIBRARIES 7 Disclaimer: The views expressed in this thesis are those of the author and do not .reflect the official policy or position of the United States Air Force, the United States Department of Defense, or the United States Government. 2 A Systems Analysis of CubeSat Constellations with Distributed Sensors by Ayesha Georgina Hein Submitted to the Department of Aeronautics and Astronautics on May 25, 2017, in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics Abstract This thesis explores the use of CubeSat constellations as "gap fillers" and supple- ments to traditionally complex, multi-sensored satellites, increasing resiliency of the system at very low cost. In standard satellite acquisitions, satellites can take years and billions of dollars to reach operational status. Should there be delays in schedule or on-orbit failures, gaps in data integral to US operations can be lost. -
IAC-18-B2.1.7 Page 1 of 16 a Technical Comparison of Three
A Technical Comparison of Three Low Earth Orbit Satellite Constellation Systems to Provide Global Broadband Inigo del Portilloa,*, Bruce G. Cameronb, Edward F. Crawleyc a Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge 02139, USA, [email protected] b Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge 02139, USA, [email protected] c Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge 02139, USA, [email protected] * Corresponding Author Abstract The idea of providing Internet access from space has made a strong comeback in recent years. After a relatively quiet period following the setbacks suffered by the projects proposed in the 90’s, a new wave of proposals for large constellations of low Earth orbit (LEO) satellites to provide global broadband access emerged between 2014 and 2016. Compared to their predecessors, the main differences of these systems are: increased performance that results from the use of digital communication payloads, advanced modulation schemes, multi-beam antennas, and more sophisticated frequency reuse schemes, as well as the cost reductions from advanced manufacturing processes (such as assembly line, highly automated, and continuous testing) and reduced launch costs. This paper compares three such large LEO satellite constellations, namely SpaceX’s 4,425 satellites Ku-Ka-band system, OneWeb’s 720 satellites Ku-Ka-band system, and Telesat’s 117 satellites Ka-band system. First, we present the system architecture of each of the constellations (as described in their respective FCC filings as of September 2018), highlighting the similarities and differences amongst the three systems. -
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O3b mPOWER Press Factsheet August 2020 O3b mPOWER As satellite plays a more prominent role in global communications, SES’s next-generation O3b mPOWER communications system builds on the proven commercial success of its current O3b Medium Earth Orbit (MEO) constellation, with breakthrough capacity, flexibility and innovations in spacecraft, ground systems, and intelligent software-driven network management, control and automation. Unlike other non-geostationary orbit satellite systems (NGSOs), the upcoming O3b mPOWER system is fully-funded, built on commercially proven technology, and based on a market-proven business case, eliminating business and operational risk for customers. Originally announced in 2017 and on target to launch in 2021, O3b mPOWER is backed by an ecosystem of technology partners and is designed for demanding applications with mobility, telecom, government and enterprise customers. Even before launch date, O3b mPOWER has achieved development and delivery milestones and has already announced major customer wins. SUCCESS OF O3b Key details include: Originally launched in 2013 to deliver • Full system: low-latency, fibre-like managed O3b mPOWER comprises an initial constellation of 11 high-throughput andlow- services, SES’s O3b was the first latency MEO satellites, extensive ground infrastructure and intelligent software and only fully NGSO broadband constellation. With a fleet of • Capacity: 20 MEO satellites, O3b supports: Terabit-level system capacity based on dynamic ability to deliver thousands ofuncontended managed