1998 Year in Review
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TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
Protostar II Mission Overview
THE VEHICLE THE SATELLITE PROTON HISTORY PROTON DESCRIPTION Lead designer was Vladimir Chelomei, who designed it TOTAL HEIGHT with the intention of creating both a powerful rocket for 58.2 m (191 ft) military payloads and a high-performance ICBM. The program was changed, and the rocket was developed GRoss LIFT-OFF exclusively for launching spacecraft. WEIGHT 705,000 kg First named UR-500, but adopted the name (1,554,000 lb) “Proton,” which also was the name of the first PROPELLANT three payloads launched. UDMH and NTO Proton launched Russian interplanetary mis- INITIAL LAUNCH sions to the Moon, Venus, Mars, and Hal- 16 July 1965 ley’s Comet. Proton-1 Spacecraft Proton launched the Salyut space sta- PAYLOAD FAIRINGS tions, the Mir core segment and both There are multiple payload fairing designs presently the Zarya (Dawn) and Zvezda (Star) mod- qualified for flight, including ules for today’s International Space Station. standard commercial payload fairings developed specifically to First commercial Proton launch — 9 April 1996. meet the needs of our customers. First commercial Proton M Breeze M launch BREEZE M UPPER STAGE — 30 December 2002 The Breeze M is powered by one pump-fed Mission Overview gimbaled main engine that develops thrust of 20 kN (4,500 lbf). It is composed of a central core and an auxilliary propellant tank which is jettisoned in flight SATELLITE OPERATOR following depletion. The Breeze M control system includes an SES on-board computer, a three-axis gyro stabilized platform, and a www.ses.com navigation system. The quantity of propellant carried is dependent SATELLITE MANUFACTURER on specific mission requirements and is varied to maximize mission Experience ILS: Achieve Your Mission performance. -
L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
Satellite Systems
Chapter 18 REST-OF-WORLD (ROW) SATELLITE SYSTEMS For the longest time, space exploration was an exclusive club comprised of only two members, the United States and the Former Soviet Union. That has now changed due to a number of factors, among the more dominant being economics, advanced and improved technologies and national imperatives. Today, the number of nations with space programs has risen to over 40 and will continue to grow as the costs of spacelift and technology continue to decrease. RUSSIAN SATELLITE SYSTEMS The satellite section of the Russian In the post-Soviet era, Russia contin- space program continues to be predomi- ues its efforts to improve both its military nantly government in character, with and commercial space capabilities. most satellites dedicated either to civil/ These enhancements encompass both military applications (such as communi- orbital assets and ground-based space cations and meteorology) or exclusive support facilities. Russia has done some military missions (such as reconnaissance restructuring of its operating principles and targeting). A large portion of the regarding space. While these efforts have Russian space program is kept running by attempted not to detract from space-based launch services, boosters and launch support to military missions, economic sites, paid for by foreign commercial issues and costs have lead to a lowering companies. of Russian space-based capabilities in The most obvious change in Russian both orbital assets and ground station space activity in recent years has been the capabilities. decrease in space launches and corre- The influence of Glasnost on Russia's sponding payloads. Many of these space programs has been significant, but launches are for foreign payloads, not public announcements regarding space Russian. -
1. INTRODUCTION 2. EASY INSTALLATION GUIDE 8. Explain How to Download S/W by USB and How to Upload and Download 9. HOW to DOWNLO
1. INTRODUCTION Overview…………………………………………………………………………..………………...……... 2 Main Features……………………………………………………………………………... ...………... ....4 2. EASY INSTALLATION GUIDE...…………...…………...…………...…………...……….. .. 3 3. SAFETY Instructions.………………………………………………………………………… …6 4. CHECK POINTS BEFORE USE……………………………………………………………… 7 Accessories Satellite Dish 5. CONTROLS/FUNCTIONS……………………………………………………………………….8 Front/Rear panel Remote controller Front Display 6. EQUIPMENT CONNECTION……………………………………………………………....… 11 CONNECTION WITH ANTENNA / TV SET / A/V SYSTEM 7. OPERATION…………………………………………………………………….………………….. 12 Getting Started System Settings Edit Channels EPG CAM(COMMON INTERFACE MODULE) Only CAS(CONDITIONAL ACCESS SYSTEM) USB Menu PVR Menu 8. Explain how to download S/W by USB and how to upload and download channels by USB……………………….……………………………………….…………………31 9. HOW TO DOWNLOAD SOFTWARE FROM PC TO RECEIVER…………….…32 10. Trouble Shooting……………………….……………………………………….………………34 11. Specifications…………………………………………………………………….……………….35 12. Glossary of Terms……………………………………………………………….……………...37 1 INTRODUCTION OVERVIEW This combo receiver is designed for using both free-to-air and encrypted channel reception. Enjoy the rich choice of more than 20,000 different channels, broadcasting a large range of culture, sports, cinema, news, events, etc. This receiver is a technical masterpiece, assembled with the highest qualified electronic parts. MAIN FEATURES • High Definition Tuners : DVB-S/DVB-S2 Satellite & DVB-T Terrestrial Compliant • DVB-S/DVB-S2 Satellite Compliant(MPEG-II/MPEG-IV/H.264) -
The International Space Station and the Space Shuttle
Order Code RL33568 The International Space Station and the Space Shuttle Updated November 9, 2007 Carl E. Behrens Specialist in Energy Policy Resources, Science, and Industry Division The International Space Station and the Space Shuttle Summary The International Space Station (ISS) program began in 1993, with Russia joining the United States, Europe, Japan, and Canada. Crews have occupied ISS on a 4-6 month rotating basis since November 2000. The U.S. Space Shuttle, which first flew in April 1981, has been the major vehicle taking crews and cargo back and forth to ISS, but the shuttle system has encountered difficulties since the Columbia disaster in 2003. Russian Soyuz spacecraft are also used to take crews to and from ISS, and Russian Progress spacecraft deliver cargo, but cannot return anything to Earth, since they are not designed to survive reentry into the Earth’s atmosphere. A Soyuz is always attached to the station as a lifeboat in case of an emergency. President Bush, prompted in part by the Columbia tragedy, made a major space policy address on January 14, 2004, directing NASA to focus its activities on returning humans to the Moon and someday sending them to Mars. Included in this “Vision for Space Exploration” is a plan to retire the space shuttle in 2010. The President said the United States would fulfill its commitments to its space station partners, but the details of how to accomplish that without the shuttle were not announced. The shuttle Discovery was launched on July 4, 2006, and returned safely to Earth on July 17. -
June, 2013 Mayumi Matsuura JAXA Flight Director Space Vehicle Technology Center Japan Aerospace Exploration Agency (JAXA) Congratulations on 50Th Anniversary
June, 2013 Mayumi Matsuura JAXA Flight Director Space Vehicle Technology Center Japan Aerospace Exploration Agency (JAXA) Congratulations on 50th Anniversary 1963.6.16 2008.3.11 The fist part of Japanese Experiment Module was launched International Space Station 1984: US President Ronald Reagan proposed developing a permanently-occupied space station 1988: Governments of Canada, ESA member countries, US and Japan signed the Intergovernmental Agreement on a cooperative framework for the space station 1993: Russia joined the program 1998: Beginning of on-orbit station assembly 2000: Beginning of continuous stay of the astronauts 2008: Beginning of assembly of Japanese Experiment Module 2011: Completion of station assembly Present: In the utilization phase International Partners ISS is truly an International space collaboration effort, with the participation of many countries. (C) NASA The First Piece of ISS ISS assembly sequence started in 1998 with the Russian module, Zarya (sunrise), launched by a Russian Proton rocket vehicle. Nov. 20, 1998 Zarya provides battery power, fuel storage and rendezvous and docking capability for Soyuz and Progress space vehicles. (C) NASA ISS Under Construction...(1998-2011) Dec. 2000 Dec. 1998 Dec. 1998 Dec. 2006 (C) NASA ISS Assembly Completion July 2011, Space shuttle Atlantis, on its final spaceflight of the Space Shuttle Program, carried the Raffaello multipurpose logistics module. 2011.7@STS-135 (C) NASA Japanese Experimental Module (JEM) - Kibo Experiment Logistic Module - Pressurized Section (2008.Mar) ・ 8 racks can be installed Pressurized Module (2008. Jun) ・ Cargo storage area ・ The largest pressurized module on ISS ・ 10 payload racks can be installed ・ Various resources provided Remote Manipulator System (power, communication, thermal control, gas supply and exhaust) (2008. -
1 Before the Federal Communications Commission Washington, D.C
Federal Communications Commission DA 06-4 Before the Federal Communications Commission Washington, D.C. 20554 In the Matter of ) ) AFRISPACE, INC. ) IB File No. SAT-LOA-20050311- ) 00061 Application for Authority to Launch and ) Operate a Replacement Satellite, AfriStar-2, ) Call Sign: S2666 at 21° E.L. and to Co-locate It with AfriStar-1 ) ) ORDER AND AUTHORIZATION Adopted: January 03, 2006 Released: January 03, 2006 By the Chief, International Bureau: I. INTRODUCTION 1. By this Order, we authorize AfriSpace, Inc. (AfriSpace)1 to launch and operate the AfriStar-2 satellite in the geostationary-satellite orbit (GSO) at the 21° East Longitude (E.L.) orbital location. AfriStar-2 is controlled from the United States and is capable of providing Broadcasting-Satellite Service (sound) (BSS (sound)) to Africa and Europe on a non-common carrier basis. We authorize AfriStar-2 to operate downlinks within 2.6 megahertz of spectrum in each polarization with a center frequency of 1479.5 MHz. We also authorize AfriSpace to utilize feeder links and telecommand links for the AfriStar-2 satellite in the 7025-7075 MHz frequency band, to operate its telemetry link for the AfriStar-2 satellite at a center frequency of 1491.7 MHz, and to co-locate the AfriStar-2 satellite at 21° E.L. with the AfriStar-1 satellite currently in orbit. In addition, we grant AfriSpace a waiver of the Commission’s rule regarding transponder saturation flux densities for the AfriStar-2 satellite.2 These authorizations give AfriSpace the capability to continue to provide service to existing customers despite unanticipated technical difficulties experienced by the AfriStar-1 satellite and to serve new customers, conditioned on AfriSpace complying with the applicable laws, regulations, rules, and licensing procedures of any countries it proposes to serve. -
November 23, 2016 VIA ELECTRONIC FILING Marlene H
November 23, 2016 VIA ELECTRONIC FILING Marlene H. Dortch, Secretary Federal Communications Commission 445 12th Street, S.W. Room TW-A325 Washington, DC 20554 Re: SAT-ASG-20161025-00101 Application for Assignment of Authorizations for AfriStar-1 and AfriStar-2 (call signs S2367 and S2666) from Yazmi USA, LLC (“Yazmi”) to Silkwave Africa, LLC (“Silkwave”). Dear Ms. Dortch: At the request of FCC staff, we are submitting this letter in the docket for the above-named application (the “Application”) to supplement statements made in the Public Interest Statement of that Application. The Public Interest Statement explained that the AfriStar-1 satellite will be initially controlled by Intelsat pursuant to an agreement between Intelsat, Silkwave, and an affiliate of Silkwave. The affiliate of Silkwave referred to is New York Broadband LLC, a U.S. limited liability company (“NYBB”). NYBB is affiliated with Silkwave because Chi Capital, which owns 100% of Silkwave, also has a minority ownership interest in NYBB. NYBB owns an Australian-licensed satellite, AsiaStar, which is operated by Intelsat pursuant to an agreement between NYBB and Intelsat (the “NYBB Agreement”). The AsiaStar satellite was also acquired from Yazmi pursuant to a series of earlier transactions not requiring FCC approval. The AfriStar-1 satellite is currently being operated by Intelsat pursuant to a separate agreement between Yazmi and Intelsat (the “Yazmi Agreement”). The parties intend that, following the transfer of the AfriStar-1 license to Silkwave, Intelsat will continue to operate the AfriStar-1 satellite on Silkwave’s behalf, either through an amended Yazmi Agreement, or more likely through an amended NYBB Agreement that includes the AfriStar-1 satellite and adds Silkwave as a party. -
Journal of Space Law
JOURNAL OF SPACE LAW VOLUME 24, NUMBER 2 1996 JOURNAL OF SPACE LAW A journal devoted to the legal problems arising out of human activities in outer space VOLUME 24 1996 NUMBERS 1 & 2 EDITORIAL BOARD AND ADVISORS BERGER, HAROLD GALLOWAY, ElLENE Philadelphia, Pennsylvania Washington, D.C. BOCKSTIEGEL, KARL·HEINZ HE, QIZHI Cologne, Germany Beijing, China BOUREr.. Y, MICHEL G. JASENTULIYANA, NANDASIRI Paris, France Vienna. Austria COCCA, ALDO ARMANDO KOPAL, VLADIMIR Buenes Aires, Argentina Prague, Czech Republic DEMBLING, PAUL G. McDOUGAL, MYRES S. Washington, D. C. New Haven. Connecticut DIEDERIKS·VERSCHOOR, IE. PH. VERESHCHETIN, V.S. Baarn, Holland Moscow. Russ~an Federation FASAN, ERNST ZANOTTI, ISIDORO N eunkirchen, Austria Washington, D.C. FINCH, EDWARD R., JR. New York, N.Y. STEPHEN GOROVE, Chairman Oxford, Mississippi All correspondance should be directed to the JOURNAL OF SPACE LAW, P.O. Box 308, University, MS 38677, USA. Tel./Fax: 601·234·2391. The 1997 subscription rates for individuals are $84.80 (domestic) and $89.80 (foreign) for two issues, including postage and handling The 1997 rates for organizations are $99.80 (domestic) and $104.80 (foreign) for two issues. Single issues may be ordered for $56 per issue. Copyright © JOURNAL OF SPACE LAW 1996. Suggested abbreviation: J. SPACE L. JOURNAL OF SPACE LAW A journal devoted to the legal problems arising out of human activities in outer space VOLUME 24 1996 NUMBER 2 CONTENTS In Memoriam ~ Tribute to Professor Dr. Daan Goedhuis. (N. J asentuliyana) I Articles Financing and Insurance Aspects of Spacecraft (I.H. Ph. Diederiks-Verschoor) 97 Are 'Stratospheric Platforms in Airspace or Outer Space? (M. -
Quarterly Launch Report
Commercial Space Transportation QUARTERLY LAUNCH REPORT Featuring the launch results from the previous quarter and forecasts for the next two quarters 4th Quarter 1997 U n i t e d S t a t e s D e p a r t m e n t o f T r a n s p o r t a t i o n • F e d e r a l A v i a t i o n A d m i n i s t r a t i o n A s s o c i a t e A d m i n i s t r a t o r f o r C o m m e r c i a l S p a c e T r a n s p o r t a t i o n QUARTERLY LAUNCH REPORT 1 4TH QUARTER 1997 REPORT Objectives This report summarizes recent and scheduled worldwide commercial, civil, and military orbital space launch events. Scheduled launches listed in this report are vehicle/payload combinations that have been identified in open sources, including industry references, company manifests, periodicals, and government documents. Note that such dates are subject to change. This report highlights commercial launch activities, classifying commercial launches as one or more of the following: • Internationally competed launch events (i.e., launch opportunities considered available in principle to competitors in the international launch services market), • Any launches licensed by the Office of the Associate Administrator for Commercial Space Transportation of the Federal Aviation Administration under U.S. -
An Elementary Approach Towards Satellite Communication
AN ELEMENTARY APPROACH TOWARDS SATELLITE COMMUNICATION Prof. Dr. Hari Krishnan GOPAKUMAR Prof. Dr. Ashok JAMMI AN ELEMENTARY APPROACH TOWARDS SATELLITE COMMUNICATION Prof. Dr. Hari Krishnan GOPAKUMAR Prof. Dr. Ashok JAMMI AN ELEMENTARY APPROACH TOWARDS SATELLITE COMMUNICATION WRITERS Prof. Dr. Hari Krishnan GOPAKUMAR Prof. Dr. Ashok JAMMI Güven Plus Group Consultancy Inc. Co. Publications: 06/2021 APRIL-2021 Publisher Certificate No: 36934 E-ISBN: 978-605-7594-89-1 Güven Plus Group Consultancy Inc. Co. Publications All kinds of publication rights of this scientific book belong to GÜVEN PLUS GROUP CONSULTANCY INC. CO. PUBLICATIONS. Without the written permission of the publisher, the whole or part of the book cannot be printed, broadcast, reproduced or distributed electronically, mechanically or by photocopying. The responsibility for all information and content in this Book, visuals, graphics, direct quotations and responsibility for ethics / institutional permission belongs to the respective authors. In case of any legal negativity, the institutions that support the preparation of the book, especially GÜVEN PLUS GROUP CONSULTANCY INC. CO. PUBLISHING, the institution (s) responsible for the editing and design of the book, and the book editors and other person (s) do not accept any “material and moral” liability and legal responsibility and cannot be taken under legal obligation. We reserve our rights in this respect as GÜVEN GROUP CONSULTANCY “PUBLISHING” INC. CO. in material and moral aspects. In any legal problem/situation TURKEY/ISTANBUL courts are authorized. This work, prepared and published by Güven Plus Group Consultancy Inc. Co., has ISO: 10002: 2014- 14001: 2004-9001: 2008-18001: 2007 certificates. This work is a branded work by the TPI “Turkish Patent Institute” with the registration number “Güven Plus Group Consultancy Inc.