Industry Brief Disaster on the Launchpad Implications for Spacex
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APSCC Monthly E-Newsletter NOVEMBER 2017
APSCC Monthly e-Newsletter NOVEMBER 2017 The Asia-Pacific Satellite Communications Council (APSCC) e-Newsletter is produced on a monthly basis as part of APSCC’s information services for members and professionals in the satellite industry. Subscribe to the APSCC monthly newsletter and be updated with the latest satellite industry news as well as APSCC activities! To renew your subscription, please visit www.apscc.or.kr/sub4_5.asp. To unsubscribe, send an email to [email protected] with a title “Unsubscribe.” News in this issue has been collected from October 1 to October 31. INSIDE APSCC The APSCC 2017 Conference & Exhibition Marks Another Great Success! The APSCC 2017 Satellite Conference & Exhibition successfully ended on 12 October 2017 in Tokyo after 3 days of in-depth conference sessions, state-of-the-art technology displayed exhibition, and diverse networking events with more than 400 delegates attending the event. At APSCC 2017, thought leaders covered major issues impacting the Asia-Pacific satellite industry, including market insight on the latest trends, new applications, and innovative technical solutions throughout the three-day roundtable discussions and presentation sessions. The APSCC 2018 Satellite Conference & Exhibition will be held on 9-11 October in Jakarta, Indonesia. The APSCC-ISU Youth Development Workshop The second APSCC-ISU Youth Development Workshop was successfully held concurrently with the APSCC 2017 event on October 12. The workshop provided a platform for the brightest up-and-coming engineering students and young professionals in Japan to connect with leading satellite and space industry experts and learn more about the opportunities in the sector. -
Driving Innovation in the ATS Market (2018 Small Payload Rideshare Symposium) Bob Caffrey NASA/GSFC [email protected] June, 13, 2018
https://ntrs.nasa.gov/search.jsp?R=20180004166 2019-08-31T16:05:42+00:00Z Driving Innovation in the ATS Market (2018 Small Payload Rideshare Symposium) Bob Caffrey NASA/GSFC [email protected] June, 13, 2018 Commercial HP (SES/GOLD) Rideshare Poster‐child: DSCOVR & TESS DSCOVR: Feb 2015 TESS: April 2018 2500 kg of unused mass went to L-1 ~3000 kg excess on a TLI orbit 6/12/2018 2 Government Rideshare: Past, Present & Future 6/12/2018 Past Missions (DSCOVR) Future Multi‐missions (STP‐2) 3 NASA Mission Opportunities: (http://soma.larc.nasa.gov/standardao/pdf_files/SMDSolicitationPlanningList.pdf) Planned AO Required NASA Science Opportunity AO Release Date Launch Window Heliophysics STP‐5 AO & MOO NET Q3 FY 2017 AO + ~6.5 years Heliophysics MIDEX AO/MOO NET Q1 FY 2018 AO + ~6.5 years EVI‐5 AO (every 18 months) NET Q2 FY 2018 AO + ~6.5 years LWS (GDC) AO & MOO Q4 FY 2018 AO + ~6.5 years Astrophysics Explorers MOO NET Q4 FY 2018 AO + ~6.5 years Astrophysics SMEX NET Q2 FY 2019 AO + ~6.5 years EVM‐3 AO TBD AO + ~6.5 years 6/12/2018 4 Access to Space (ATS) Options Access to Space (ATS) Decision Tree NASA Rideshare Opportunities: Cost: Risk: Rideshare? Benefits: D4 USAF/DoD RS Opportunities: Cost: Risk: Benefits: Rideshare or Hosted P/L? Commercial RS Opportunities: Cost: Risk: D2 Benefits: NASA HP Opportunities: Cost: No Risk: Hosted P/L? Benefits: Dedicated Launch? D5 USAF/DoD HP Opportunities: Cost: Risk: Access Benefits: To Space D1 Commercial HP Opportunities: Cost: Yes Risk: Benefits: Small, Medium, Or Large L/V? Small L/V (< 5,000 -
Orbital Debris Quarterly News 22-1
National Aeronautics and Space Administration Orbital Debris Quarterly News Volume 22, Issue 1 February 2018 Inside... Two Anomalous Events in GEO Summer 2017 was marred by two apparently platform. Spacecraft dry mass is estimated to be on Space Debris Sensor anomalous events in the geosynchronous orbit the order of 2000 kg. On-board stored energy sources Launches Aboard (GEO) belt. Both incidents have been observed by include fuel and pressurized components, as well as the commercial space situation awareness providers, but as battery subsystem. SpaceX-13 2 of 26 December 2017 no debris from either event have The Indonesian GEO communications spacecraft entered the public catalog. TELKOM-1 (1999-042A, SSN catalog number 25880) SEM Analysis The GEO communications spacecraft AMC-9 experienced an energetic event on or about 25 August Results of (International Designator 2003-024A, U.S. Strategic 2017, after over 18.1 years on-orbit—3 years past Returned ISS Command [USSTRATCOM] Space Surveillance its nominal operational lifetime. An examination of Network [SSN] catalog number 27820), formerly known the Two Line Element data indicates an observable PMA-2 Cover 4 as GE-12, experienced an energetic event estimated to change in spacecraft orbit between 26 and 29 August. have occurred at approximately 07:10 GMT on 17 June At the beginning of this time interval, approximately CubeSat Study 2017, after approximately 14 years on-orbit. Fig. 1 Project Review 6 depicts the orbital evolution of the spacecraft in 2017. continued on page 2 SES, the spacecraft owner- operator, described this AMC‐9 (SSN 27820, 2003‐024A) 360 36300 Space Debris Sensor event as a “serious anomaly.” Installation 8 Following this event, the 36200 spacecraft began a westward 300 Monthly Object Type drift in the GEO belt. -
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 ....................................................................................................... -
Space Business Review 11, BSAT-3B Will Be Launched by an Kazakhstan on a Russian Soyuz Vehicle
April 2008 A monthly round-up of space industry developments for the information of our clients and friends. EADS Astrium to Acquire SSTL DISH Selects SS/L for EchoStar XV EADS Astrium announced on April 7 that it On April 22, Space Systems/Loral (SS/L), had entered into an agreement with the announced a contract to build the EchoStar University of Surrey to acquire its 80% XV direct broadcast satellite for DISH stake in Surrey Satellite Technology Network Corporation. Scheduled for launch Limited (SSTL) for an estimated £40-50 in 2010, the spacecraft will be based on million. Based in the United Kingdom, SSTL SS/L’s proven 1300 platform and is designed specializes in the design and manufacture of to support the expansion of DISH Network’s small and micro satellites, including the programming and services. Giove-A test satellite for Europe's Other April Launch Services forthcoming Galileo satellite navigation On April 14, Lockheed Martin Commercial system. The transaction, which remains Launch Services successfully launched the subject to regulatory approvals, will provide ICO G1 satellite for ICO Global the financial and industrial resources Communications (Holdings) Ltd’ from Cape required for SSTL’s expansion and future Canaveral Air Force Station in Florida on an development. It is expected that SSTL will Atlas V 421 vehicle. Built by SS/L based on remain an independent UK company. its 1300 platform, ICO G1 weighed BSAT-3b Contract Awards approximately 6,634 kg at launch, is equipped On April 15, Lockheed Martin Commercial with a 12-meter S-band reflector capable of Space Systems announced its selection by ground-based beam forming that, along with a Japanese satellite operator Broadcasting complementary network of terrestrial Satellite System Corporation (B-SAT) to repeaters, will provide between 10-15 build its next broadcast satellite, designated channels of live television, enhanced BSAT-3b. -
Spaceflight, Inc. General Payload Users Guide
Spaceflight, Inc. SF‐2100‐PUG‐00001 Rev F 2015‐22‐15 Payload Users Guide Spaceflight, Inc. General Payload Users Guide 3415 S. 116th St, Suite 123 Tukwila, WA 98168 866.204.1707 spaceflightindustries.com i Spaceflight, Inc. SF‐2100‐PUG‐00001 Rev F 2015‐22‐15 Payload Users Guide Document Revision History Rev Approval Changes ECN No. Sections / Approved Pages CM Date A 2011‐09‐16 Initial Release Updated electrical interfaces and launch B 2012‐03‐30 environments C 2012‐07‐18 Official release Updated electrical interfaces and launch D 2013‐03‐05 environments, reformatted, and added to sections Updated organization and formatting, E 2014‐04‐15 added content on SHERPA, Mini‐SHERPA and ISS launches, updated RPA CG F 2015‐05‐22 Overall update ii Spaceflight, Inc. SF‐2100‐PUG‐00001 Rev F 2015‐22‐15 Payload Users Guide Table of Contents 1 Introduction ........................................................................................................................... 7 1.1 Document Overview ........................................................................................................................ 7 1.2 Spaceflight Overview ....................................................................................................................... 7 1.3 Hardware Overview ......................................................................................................................... 9 1.4 Mission Management Overview .................................................................................................... 10 2 Secondary -
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. -
Spacex Rocket Data Satisfies Elementary Hohmann Transfer Formula E-Mail: [email protected] and [email protected]
IOP Physics Education Phys. Educ. 55 P A P ER Phys. Educ. 55 (2020) 025011 (9pp) iopscience.org/ped 2020 SpaceX rocket data satisfies © 2020 IOP Publishing Ltd elementary Hohmann transfer PHEDA7 formula 025011 Michael J Ruiz and James Perkins M J Ruiz and J Perkins Department of Physics and Astronomy, University of North Carolina at Asheville, Asheville, NC 28804, United States of America SpaceX rocket data satisfies elementary Hohmann transfer formula E-mail: [email protected] and [email protected] Printed in the UK Abstract The private company SpaceX regularly launches satellites into geostationary PED orbits. SpaceX posts videos of these flights with telemetry data displaying the time from launch, altitude, and rocket speed in real time. In this paper 10.1088/1361-6552/ab5f4c this telemetry information is used to determine the velocity boost of the rocket as it leaves its circular parking orbit around the Earth to enter a Hohmann transfer orbit, an elliptical orbit on which the spacecraft reaches 1361-6552 a high altitude. A simple derivation is given for the Hohmann transfer velocity boost that introductory students can derive on their own with a little teacher guidance. They can then use the SpaceX telemetry data to verify the Published theoretical results, finding the discrepancy between observation and theory to be 3% or less. The students will love the rocket videos as the launches and 3 transfer burns are very exciting to watch. 2 Introduction Complex 39A at the NASA Kennedy Space Center in Cape Canaveral, Florida. This launch SpaceX is a company that ‘designs, manufactures and launches advanced rockets and spacecraft. -
PRFP-11) & Interconnectivity Workshop 26-30 November 2019, Apia, SAMOA
11th APT Policy and Regulation Forum for Pacific (PRFP-11) & Interconnectivity Workshop 26-30 November 2019, Apia, SAMOA Workshop Topic ENABLERS FOR A BETTER CONNECTED PACIFIC - New Satellite Technologies and Services (MSS, ESIM and LEOs) Dr Bob Horton Consultant Satellite Industry ENABLERS FOR A BETTER CONNECTED PACIFIC - New Satellite Technologies and Services (MSS and LEOs) CONTENTS • Examples of progress : MSS, ESIM – Inmarsat LEOs – OneWeb • Pacific Needs - understanding and participating in the regional/global environment - the Pacific : a “Collection of Islands” or an “Island Collective”? - opportunities overdue in APAC Inmarsat use of spectrum L band Ka band User links: 1626.5-1660.5 MHz ↑, 1525-1559 Feeder link ↑ : 27.5 – 30.0 GHz MHz↓ Feeder link↓ : 17.7 – 20.2 GHz Extended L-band: User link ↑ : 29.0 – 30.0 GHz User link↓ : 19.2 – 20.2 GHz User links: 1668-1675 MHz ↑, 1518 MHz-1525 MHz ↓ Used by Inmarsat Global Express satellites S band Used by Inmarsat-4 satellites and Alphasat Feeder link ↑ : 27.5 – 29.5 GHz Feeder link↓ : 17.7 – 19.7 GHz User link ↑ 1980-2010MHz Q/V band User link↓ : 2170-2200MHz C band 37.5-42.5 GHz ↓ Used by Europasat Feeder links for L-band satellites operate in 47.2-50.2 GHz + 50.4-51.4 GHz ↑ the bands 3550 – 3700 MHz and 6425 – - Planned for future satellites to free 6575 MHz through more than 20 Land Earth Stations up Ka-band for user terminals TT&C operated in standard C-band on most - Developmental payload on Alphasat Inmarsat satellites Inmarsat and Extended L-band Extended L-band will be available -
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 . -
GOLDBERG, GODLES, WIENER & WRIGHT LLP November 2, 2015
LAW OFFICES GOLDBERG, GODLES, WIENER & WRIGHT LLP 1229 NINETEENTH STREET, N.W. WASHINGTON, D.C. 20036-2413 HENRY GOLDBERG (202) 429-4900 JOSEPH A. GODLES TELECOPIER: JONATHAN L. WIENER (202) 429-4912 DEVENDRA (“DAVE”) KUMAR e-mail: ________ [email protected] HENRIETTA WRIGHT website: www.g2w2.com THOMAS G. GHERARDI, P.C. COUNSEL ________ THOMAS S. TYCZ* SENIOR POLICY ADVISOR *NOT AN ATTORNEY November 2, 2015 BY ELECTRONIC FILING Mr. Jose P. Albuquerque Chief, Satellite Division International Bureau Federal Communications Commission Washington, D.C. 20554 Re: Spaceflight, Inc. Request for Special Temporary Authority IBFS File No. SAT-STA-20150821-00060 Dear Mr. Albuquerque: Spaceflight, Inc. (“Spaceflight”), by its counsel, responds to your letter of October 6, 2015, in which the International Bureau seeks additional information related to Spaceflight’s above-referenced application for Special Temporary Authority (“STA”) to communicate with its SHERPA spacecraft. We are hereby transmitting by IBFS responses to the Bureau’s questions. In addition, we are transmitting material that supplements and updates the Orbital Debris Assessment Report that was submitted with the original application request. Spaceflight also hereby notifies the Bureau that the proposed timeframe of the SHERPA mission has shifted. In its original request, Spaceflight stated that, because of recent delays and uncertainties in the space launch industry, it was requesting STA to cover a timeframe of three months – January 15, 2016 to April 15, 2016 – during which its SHERPA mission was expected to occur. Based upon the most recent information available, Spaceflight expects its SHERPA spacecraft instead to be launched as a single occurrence between March 15, 2015 and June 15, 2015.