DOCSLIB.ORG

Booster Versionlaunch Site Payload Customer Outcome 1 4/6

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Booster Versionlaunch Site Payload Customer Outcome 1 4/6 Flight Numb Date Time (UTC) Booster VersionLaunch Site Payload Customer Outcome 1 4/6/10 18:45:00 F9 v1.0 B0003CCAFS LC-40 Dragon Spacecraft Qualification Unit SpaceX Success 2 8/12/10 15:43:00 F9 v1.0 B0004CCAFS LC-40 Dragon demo flight C1, two CubeSats NASA (COTS) NRO Success 3 22/5/12 7:44:00 F9 v1.0 B0005CCAFS LC-40 Dragon demo flight C2+ NASA (COTS) Success 4 8/10/12 0:35:00 F9 v1.0 B0006CCAFS LC-40 SpaceX CRS-1 NASA (CRS) Failure 5 1/3/13 15:10:00 F9 v1.0 B0007CCAFS LC-40 SpaceX CRS-2 NASA (CRS) Success 6 29/9/13 16:00:00 F9 v1.1 B1003VAFB SLC-4E CASSIOPE MDA Success 7 3/12/13 22:41:00 F9 v1.1 CCAFS LC-40 SES-8 SES Success 8 6/1/14 22:06:00 F9 v1.1 CCAFS LC-40 Thaicom 6 Thaicom Success 9 18/4/14 19:25:00 F9 v1.1 CCAFS LC-40 SpaceX CRS-3 NASA (CRS) Success 10 14/7/14 15:15:00 F9 v1.1 CCAFS LC-40 OG2 Mission 1 6 Orbcomm-OG2 satellites Orbcomm Success 11 5/8/14 8:00:00 F9 v1.1 CCAFS LC-40 AsiaSat 8 AsiaSat Success 12 7/9/14 5:00:00 F9 v1.1 B1011CCAFS LC-40 AsiaSat 6 AsiaSat Success 13 21/9/14 5:52:00 F9 v1.1 B1010CCAFS LC-40 SpaceX CRS-4 NASA (CRS) Success 14 10/1/15 9:47:00 F9 v1.1 B1012CCAFS LC-40 SpaceX CRS-5 NASA (CRS) Success 15 11/2/15 23:03:00 F9 v1.1 B1013CCAFS LC-40 DSCOVR U.S. Air Force Success 16 2/3/15 3:50:00 F9 v1.1 B1014CCAFS LC-40 ABS-3A Eutelsat 115 West B ABS Eutelsat Success 17 14/4/15 20:10:00 F9 v1.1 B1015CCAFS LC-40 SpaceX CRS-6 NASA (CRS) Success 18 27/4/15 23:03:00 F9 v1.1 B1016CCAFS LC-40 TürkmenÄlem 52°E / MonacoSAT Turkmenistan Success 19 28/6/15 14:21:00 F9 v1.1 B1018CCAFS LC-40 SpaceX CRS-7 NASA (CRS) Failure 20 22/12/15 1:29:00 F9 FT B1019 CCAFS LC-40 OG2 Mission 2 11 Orbcomm-OG2 satellites Orbcomm Success 21 17/1/16 18:42:00 F9 v1.1 B1017VAFB SLC-4E Jason-3 NASA (LSP) Success 22 4/3/16 23:35:00 F9 FT B1020 CCAFS LC-40 SES-9 SES Success 23 8/4/16 20:43:00 F9 FT B1021.1CCAFS LC-40 SpaceX CRS-8 NASA (CRS) Success 24 6/5/16 5:21:00 F9 FT B1022 CCAFS LC-40 JCSAT-14 SKY Perfect Success 25 27/5/16 21:39:00 F9 FT B1023.1CCAFS LC-40 Thaicom 8 Thaicom Success 26 15/6/16 14:29:00 F9 FT B1024 CCAFS LC-40 ABS-2A Eutelsat 117 West B ABS Eutelsat Success 27 18/7/16 4:45:00 F9 FT B1025.1CCAFS LC-40 SpaceX CRS-9 NASA (CRS) Success 28 14/8/16 5:26:00 F9 FT B1026 CCAFS LC-40 JCSAT-16 SKY Perfect Success 29 14/1/17 17:54:00 F9 FT B1029.1VAFB SLC-4E Iridium NEXT 1 Iridium Success 30 19/2/17 14:39:00 F9 FT B1031.1KSC LC-39A SpaceX CRS-10 NASA (CRS) Success 31 16/3/17 6:00:00 F9 FT B1030 KSC LC-39A EchoStar 23 EchoStar Success 32 30/3/17 22:27:00 F9 FT B1021.2KSC LC-39A SES-10 SES Success 33 1/5/17 11:15:00 F9 FT B1032.1KSC LC-39A NROL-76 NRO Success 34 15/5/17 23:21:00 F9 FT B1034 KSC LC-39A Inmarsat-5 F4 Inmarsat Success 35 3/6/17 21:07:00 F9 FT B1035.1KSC LC-39A SpaceX CRS-11 NASA (CRS) Success 36 23/6/17 19:10:00 F9 FT B1029.2KSC LC-39A BulgariaSat-1 Bulsatcom Success 37 25/6/17 20:25:00 F9 FT B1036.1VAFB SLC-4E Iridium NEXT 2 Iridium Communications Success 38 5/7/17 23:38:00 F9 FT B1037 KSC LC-39A Intelsat 35e Intelsat Success 39 14/8/17 16:31:00 F9 B4 B1039.1KSC LC-39A SpaceX CRS-12 NASA (CRS) Success 40 24/8/17 18:51:00 F9 FT B1038.1VAFB SLC-4E Formosat-5 NSPO Success 41 7/9/17 14:00:00 F9 B4 B1040.1KSC LC-39A Boeing X-37B OTV-5 U.S. Air Force Success 42 9/10/17 12:37:00 F9 B4 B1041.1VAFB SLC-4E Iridium NEXT 3 Iridium Communications Success 43 11/10/17 22:53:00 F9 FT B1031.2KSC LC-39A SES-11 / EchoStar 105 SES EchoStar Success 44 30/10/17 19:34:00 F9 B4 B1042.1KSC LC-39A Koreasat 5A KT Corporation Success 45 15/12/17 15:36:00 F9 FT B1035.2CCAFS SLC-40 SpaceX CRS-13 NASA (CRS) Success 46 23/12/17 1:27:00 F9 FT B1036.2VAFB SLC-4E Iridium NEXT 4 Iridium Communications Success 47 8/1/18 1:00:00 F9 B4 B1043.1CCAFS SLC-40 Zuma Northrop Grumman Success 48 31/1/18 21:25:00 F9 FT B1032.2CCAFS SLC-40 GovSat-1 / SES-16 SES Success 49 22/2/18 14:17:00 F9 FT B1038.2VAFB SLC-4E Paz Tintin A & B Hisdesat exactEarth SpaceX Success 50 6/3/18 5:33:00 F9 B4 B1044 CCAFS SLC-40 Hispasat 30W-6 PODSat Hispasat NovaWurks Success 51 30/3/18 14:14:00 F9 B4 B1041.2VAFB SLC-4E Iridium NEXT 5 Iridium Communications Success 52 2/4/18 20:30:00 F9 B4 B1039.2CCAFS SLC-40 SpaceX CRS-14 NASA (CRS) Success 53 18/4/18 22:51:00 F9 B4 B1045.1CCAFS SLC-40 Transiting Exoplanet Survey Satellite (TESS) NASA (LSP) Success 54 11/5/18 20:14:00 F9 B5 B1046.1KSC LC-39A Bangabandhu-1 Thales-Alenia/BTRC Success 55 22/5/18 19:47:58 F9 B4 B1043.2VAFB SLC-4E Iridium NEXT 6 GRACE-FO 1, 2 Iridium Success 56 4/6/18 4:45:00 F9 B4 B1040.2CCAFS SLC-40 SES-12 SES Success.
Load more

Recommended publications
  • Electric Propulsion for Station Keeping and Electric Orbit Raising on Eutelsat Platforms
    Electric Propulsion for Station Keeping and Electric Orbit Raising on Eutelsat Platforms 2015-b/IEPC-97 Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th International Electric Propulsion Conference and 6th Nano-satellite Symposium, Hyogo-Kobe, Japan July 4 – 10, 2015 C. Casaregola1 Eutelsat, Paris, 75015, France Abstract: With a fleet of 34 geostationary satellites and more than 30 years of service from space, Eutelsat is today Europe’s most long-standing satellite operator and one of the world’s leading satellite operators. The first two platforms using Electric Propulsion procured are SESAT-1 (EUTELSAT 16C) and KA-SAT, for which Electric Propulsion is limited to on-station operations. The successful demonstration of sustained capability of Electric Propulsion for these two platforms in addition to the extensive flight heritage with no significant anomalies demonstrated in the last decades on both commercial and scientific platforms, prove the high level of maturity reached by Electric Propulsion systems. Based on that and due to new attractive launch options, one full-electric platform - EUTELSAT 115 West B – has been procured and launched in March 2015. The launch of EUTELSAT 115 West B is a key milestone for telecom platforms as it makes Eutelsat the first Operator to use Electric Propulsion for a complete electric orbit raising. Two additional platforms – EUTELSAT 117 West B and EUTELSAT 172 B - are under procurement and will perform complete electric orbit raising as well. An overview of Eutelsat platforms using Electric Propulsion for station keeping and electric orbit raising is given in the paper.
    [Show full text]
  • October 2020 Worldwide Satellite Magazine
    Worldwide Satellite Magazine SatMagazineSatMagazine October 2020 SATELLITE ELEVATE YOUR VIRTUAL EXPECTATIONS! INNOVATION A Full Agenda, Providing Deep Insights into the Satellite Business Domain One-on-One Video Chat with Conference Attendees, Exhibitors, Sponsors and Speakers Connect With Experts Through Mutual Common Interests Meetings Find Industry Experts in Sessions, Exhibitions And Through Interest Group Search Build Your Event Calendar With Integrated Scheduling & Meeting Invitation Functions SATINNOVATION.COM October 6th-8th 2020 Experience Matters Ask us about Q- and V-band! Catch the Ka-band wave with CPI WATTS BANDWIDTH TECHNOLOGY 80-160 Ka Up to 2 GHz* GaN BUC or n More than 5,000 Ka-band HPAs and Solid State BUCs fielded SSPA n Largest selection of Ka-band amplifiers available 50-650 Ka Up to 4 GHz TWTA 800 Ka Up to 300 MHz Klystron PA n Field proven, outstanding reliability 180 Q Up to 2 GHz TWTA n Worldwide Ka-ready regional service centers 250 Pk V Up to 4.2 GHz TWTA *Two 1 GHz selectable bands Download our app! Search: CPI Satcom CPI SMP Satcom Products | www.cpii.com | [email protected] | +1 (669) 275-2744 Publishing Operations Senior Columnists This Issue’s Authors Silvano Payne, Publisher + Executive Writer Chris Forrester, Broadgate Publications Martyn Acreman HU Hai Simon Payne, Chief Technical Officer Karl Fuchs, iDirect Government Services Brad Bode Mike McNally Hartley G. Lesser, Editorial Director Bob Gough, Goonhilly Earth Station Rob Coleman Alex Miller Pattie Lesser, Executive Editor Rebecca M. Cowen-Hirsch, Inmarsat Kevin Corbley Tore Morten Olsen Donald McGee, Production Manager Ken Peterman, Viasat Chris Forrester Brian Rider Andy Bernard, Sales Director Giles Peeters, Track24 Defence Chris Formeller Bob Stanton Teresa Sanderson, Operations Director Koen Willems, ST Engineering Newtec Simon Gwozdz Dana Turse Sean Payne, Business Development Director Dan Makinster, Technical Advisor Features Advertiser Index The Forrester Report: OneWeb—One Step Forward… But… .
    [Show full text]
  • Secretariat Distr.: General 3 August 2015 English
    United Nations ST/SG/SER.E/744 Secretariat Distr.: General 3 August 2015 English Original: Spanish 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 8 April 2015 from the Permanent Mission of Mexico to the United Nations (Vienna) addressed to the Secretary-General The Permanent Mission of Mexico to the United Nations (Vienna), in accordance with articles III and IV of the Convention on Registration of Objects Launched into Outer Space (General Assembly resolution 3235 (XXIX), annex), has the honour to inform the Secretary-General of the entry into its national registry of the Mexican satellite Eutelsat 115 West B (E115WB), whose owner is the company Satélites Mexicanos, S.A. de C.V. (Eutelsat Americas) (see annex). The satellite has already been registered in the database maintained by the Mexican Space Agency. V.15-05497 (E) 140815 170815 *1505497* ST/SG/SER.E/744 Annex Registration data on a space object launched by Mexico* E115WB (Satmex 7) State of registry: Mexico Name of the space object: E115WB (Satmex 7) Date and territory or location of launch: 1 March 2015 UTC/GMT-4 Launch Complex 40 (SLC-40), Cape Canaveral Air Force Station, Florida, United States of America Basic orbital parameters Geostationary orbit location: 114.9 degrees West Inclination: 0 ± 0.05 degrees Longitudinal tolerance: ± 0.05 degrees General function of space object: Communications satellite Date of decay/re-entry/deorbit: 20 December 2030 (expected date) Additional voluntary information for use in the Register of Objects Launched into Outer Space Space object owner or operator: Satélites Mexicanos, S.A.
    [Show full text]
  • Britain Back in Space
    Spaceflight A British Interplanetary Society Publication Britain back in Space Vol 58 No 1 January 2016 £4.50 www.bis-space.com 1.indd 1 11/26/2015 8:30:59 AM 2.indd 2 11/26/2015 8:31:14 AM CONTENTS Editor: Published by the British Interplanetary Society David Baker, PhD, BSc, FBIS, FRHS Sub-editor: Volume 58 No. 1 January 2016 Ann Page 4-5 Peake on countdown – to the ISS and beyond Production Assistant: As British astronaut Tim Peake gets ready for his ride into space, Ben Jones Spaceflight reviews the build-up to this mission and examines the Spaceflight Promotion: possibilities that may unfold as a result of European contributions to Suszann Parry NASA’s Orion programme. Spaceflight Arthur C. Clarke House, 6-9 Ready to go! 27/29 South Lambeth Road, London, SW8 1SZ, England. What happens when Tim Peake arrives at the International Space Tel: +44 (0)20 7735 3160 Station, where can I watch it, listen to it, follow it, and what are the Fax: +44 (0)20 7582 7167 broadcasters doing about special programming? We provide the Email: [email protected] directory to a media frenzy! www.bis-space.com 16-17 BIS Technical Projects ADVERTISING Tel: +44 (0)1424 883401 Robin Brand has been busy gathering the latest information about Email: [email protected] studies, research projects and practical experiments now underway at DISTRIBUTION the BIS, the first in a periodic series of roundups. Spaceflight may be received worldwide by mail through membership of the British 18 Icarus Progress Report Interplanetary Society.
    [Show full text]
  • FCC-21-49A1.Pdf
    Federal Communications Commission FCC 21-49 Before the Federal Communications Commission Washington, DC 20554 In the Matter of ) ) Assessment and Collection of Regulatory Fees for ) MD Docket No. 21-190 Fiscal Year 2021 ) ) Assessment and Collection of Regulatory Fees for MD Docket No. 20-105 Fiscal Year 2020 REPORT AND ORDER AND NOTICE OF PROPOSED RULEMAKING Adopted: May 3, 2021 Released: May 4, 2021 By the Commission: Comment Date: June 3, 2021 Reply Comment Date: June 18, 2021 Table of Contents Heading Paragraph # I. INTRODUCTION...................................................................................................................................1 II. BACKGROUND.....................................................................................................................................3 III. REPORT AND ORDER – NEW REGULATORY FEE CATEGORIES FOR CERTAIN NGSO SPACE STATIONS ....................................................................................................................6 IV. NOTICE OF PROPOSED RULEMAKING .........................................................................................21 A. Methodology for Allocating FTEs..................................................................................................21 B. Calculating Regulatory Fees for Commercial Mobile Radio Services...........................................24 C. Direct Broadcast Satellite Regulatory Fees ....................................................................................30 D. Television Broadcaster Issues.........................................................................................................32
    [Show full text]
  • System Analysis and Design of the Geostationary Earth Orbit All-Electric Communication Satellites
    https://doi.org/10.1590/jatm.v13.1205 REVIEW ARTICLE System Analysis and Design of the Geostationary Earth Orbit All-Electric Communication Satellites Parsa Abbasrezaee1,* , Ali Saraaeb2 1.Sapienza University of Rome – Aerospace Engineering School – Rome – Italy. 2.Khaje Nasir Toosi University of Technology – Aerospace department – Tehran – Iran. *Corresponding author: [email protected] ABSTRACT With the help of gathered data and formulas extracted from a previous conference paper, the all-electric geostationary Earth orbit (GEO) communication satellite statistical design was conducted and further studied with analytic hierarchy process (AHP) and technique for order of preference by similarity to ideal solution (TOPSIS) methods. Moreover, with the help of previously determined system parameters, the orbital ascension, orbital maintenance and deorbiting specifications, calculations and simulations were persuaded. Furthermore, a parametric subsystem design was conducted to test the methods reliability and prove the feasibility of such approach. The parametric subsystem design was used for electrical power subsystem (EPS), attitude determination and control system (ADCS), electric propulsion, telemetry, tracking and control (TT&C) in conceptual subsystem design level, which highly relies on the satellite type and other specifications, were concluded in this paper; other subsystem designs were not of a significant difference to hybrid and chemical satellites. Eventually, the verification of the mentioned subsystems has been evaluated by contrasting the results with the Space mission engineering: the new SMAD, and subsystem design book reference. Keywords: All-electric; GEO; AHP and TOPSIS Method; Maintenance; Deorbiting; Parametric. INTRODUCTION From the previous conference paper, the contrast between all-electric geostationary Earth orbit (GEO) communication and other hybrid and chemical satellite design has shown that using all-electric satellite design has many advantages.
    [Show full text]
  • 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).
    [Show full text]
  • ESOG 120 Issue 8 – Rev
    TYPE APPROVAL AND CHARACTERIZATION PROCEDURES ESOG 120 Issue 8 – Rev. 1, May 2021 Antennas and Transmissions Team Antenna and VSAT Type Approval/Characterization ESOG 120 – Issue 8 - Rev. 1 May 2021 Antennas and VSATs Type Approval / Characterization Table of Contents Forward .................................................................................................................................. v 1 Overview of the ESOG modules ...................................................................................... 6 1.1 Volume I: Eutelsat S.A. system management and policies ........................................................ 6 1.2 Volume II: Eutelsat S.A. system operations and procedures ..................................................... 6 2 Introduction ................................................................................................................... 7 2.1 About this document .................................................................................................................. 7 2.2 Disclaimer ................................................................................................................................... 7 2.3 Eutelsat certification .................................................................................................................. 7 2.3.1 Type Approval ........................................................................................................................ 8 2.3.2 Characterization ....................................................................................................................
    [Show full text]
  • Space Propulsion Technology for Small Spacecraft
    Space Propulsion Technology for Small Spacecraft The MIT Faculty has made this article openly available. Please share how this access benefits you. Your story matters. Citation Krejci, David, and Paulo Lozano. “Space Propulsion Technology for Small Spacecraft.” Proceedings of the IEEE, vol. 106, no. 3, Mar. 2018, pp. 362–78. As Published http://dx.doi.org/10.1109/JPROC.2017.2778747 Publisher Institute of Electrical and Electronics Engineers (IEEE) Version Author's final manuscript Citable link http://hdl.handle.net/1721.1/114401 Terms of Use Creative Commons Attribution-Noncommercial-Share Alike Detailed Terms http://creativecommons.org/licenses/by-nc-sa/4.0/ PROCC. OF THE IEEE, VOL. 106, NO. 3, MARCH 2018 362 Space Propulsion Technology for Small Spacecraft David Krejci and Paulo Lozano Abstract—As small satellites become more popular and capa- While designations for different satellite classes have been ble, strategies to provide in-space propulsion increase in impor- somehow ambiguous, a system mass based characterization tance. Applications range from orbital changes and maintenance, approach will be used in this work, in which the term ’Small attitude control and desaturation of reaction wheels to drag com- satellites’ will refer to satellites with total masses below pensation and de-orbit at spacecraft end-of-life. Space propulsion 500kg, with ’Nanosatellites’ for systems ranging from 1- can be enabled by chemical or electric means, each having 10kg, ’Picosatellites’ with masses between 0.1-1kg and ’Fem- different performance and scalability properties. The purpose tosatellites’ for spacecrafts below 0.1kg. In this category, the of this review is to describe the working principles of space popular Cubesat standard [13] will therefore be characterized propulsion technologies proposed so far for small spacecraft.
    [Show full text]
  • FIRST QUARTER 2015-2016 REVENUES Wednesday 28Th October 2015 Agenda
    FIRST QUARTER 2015-2016 REVENUES Wednesday 28th October 2015 Agenda Business highlights Q1 2015-2016 performance Outlook 2 Business highlights Q1 revenues up 8.4% and 2.0% at constant currency putting us on track to deliver full-year objectives Several contracts signed in in all geographies and applications contributing to an order book of €6.0bn Successful launch and entry into service of EUTELSAT 8 West B boosting MENA coverage Entry into service ahead of schedule of EUTELSAT 115 West B bringing additional resources in LATAM Launch of African Broadband initiative . Lease of AMOS-6 Ka-band payload in partnership with Facebook . Procurement of a follow-on stand-alone HTS Satellite Launch of “Future Video Initiative” with SES to advance the adaptation of the satellite industry to evolving video landscapes 3 Agenda Business highlights Q1 2015-2016 performance Outlook 4 Q1 revenues: €388m, +2.0% at constant currency1 REVENUE REVENUES3 Y-O-Y CHANGE (%) CONTRIBUTION2 (€m) AT CONSTANT ACTUAL CURRENCY 62% 229 -1.6 +0.8 Video 16% 59 -0.3 +14.9 Data 8% 30 +12.4 +13.1 VASVAS VAS Government 14% 53 -0.7 +19.2 Services 1 + 8.4% at actual rate 2 The share of each application as a percentage of total revenues is calculated excluding “other revenues” and “non-recurring revenues”. 3 Total revenues of €387.7m also include Other revenues of €16.7m 5 Video: Slight decline in revenues, awaiting new capacity Revenues of €229m down 1.6% at constant currency1 Revenues Good performance of Eutelsat Americas, 7° (€m) East and 16° East 913 Ongoing impact of non-renewal at HOT BIRD of contracts with some service providers Q4 235 Renegotiation of Russian contracts 5,855 channels broadcast at end-September Q3 225 2015 Q2 225 HD penetration at 12.3% vs.
    [Show full text]
  • Aleutian Broadband Scoping Study
    Aleutian Broadband Scoping Study Prepared for The Southwest Alaska Municipal Conference (SWAMC) March 2018 3940 Arctic Blvd., Suite 102 Anchorage, Alaska 99503 Phone: (907) 677-2601 Fax: (907) 677-2605 www.meridianak.com E-mail: [email protected] Preparers Erik Fredeen Shawn Fitzpatrick Cyrinda Hoffman Johnathon Storter James Burkhart Cover Photos: 1. SEAFAST Project, Photo by Meridian Management 2. TERRA-Southwest Project, Photo by Meridian Management 3. TERRA- Southwest Project, Photo by Meridian Management 4. Satellite Earth Station, Photo by GCI Contents Abbreviations ................................................................................................................................................ v Executive Summary ................................................................................................................................ ES-1 1 Introduction ........................................................................................................................................... 1 1.1 Background and Goals of this Report ........................................................................................... 1 1.2 Study Area .................................................................................................................................... 2 1.3 Demographics ............................................................................................................................... 2 1.3.1 Existing Population ..............................................................................................................
    [Show full text]
  • FCC-21-98A1.Pdf
    Federal Communications Commission FCC 21-98 Before the Federal Communications Commission Washington, D.C. 20554 In the Matter of ) ) Assessment and Collection of Regulatory Fees for ) MD Docket No. 21-190 Fiscal Year 2021 ) ) REPORT AND ORDER AND NOTICE OF PROPOSED RULEMAKING Adopted: August 25, 2021 Released: August 26, 2021 Comment Date: [30 days after date of publication in the Federal Register] Reply Comment Date: [45 days after date of publication in the Federal Register] By the Commission: Acting Chairwoman Rosenworcel and Commissioners Carr and Simington issuing separate statements. TABLE OF CONTENTS Heading Paragraph # I. INTRODUCTION...................................................................................................................................1 II. BACKGROUND.....................................................................................................................................2 III. REPORT AND ORDER..........................................................................................................................6 A. Allocating Full-time Equivalents......................................................................................................7 B. Commercial Mobile Radio Service Regulatory Fees Calculation ..................................................27 C. Direct Broadcast Satellite Fees .......................................................................................................28 D. Full-Service Television Broadcaster Fees ......................................................................................36
    [Show full text]