DOCSLIB.ORG

AXM ISS Russian Segment 1:100

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
AXM ISS Russian Segment 1:100 AXM International Space Station 1:100 scale combo kit #3 (Russian Segment) Contents: ZARYA and Docking Target ZVEZDA Service Module PIRS (DC-1) POISK (MRM-2) RASSVET (MRM-1) 5 Debri panels for small diameter of Zvezda ©2013 Print on Cardstock (110 lbs) 1 cm KOMPAACT 2 Zarya 1 inch 1:100 Scale AKP BKA 1 BKA AKP om PMA CM 3 3 CM cut AKP-BKA cut Stb P Stb P y 3 4 1 TOP 2 B1 A1 FA OFB glue FA OFB glue PMA CMom FA OFB ©2011 Not for commercial use 1 cm Print on Cardstock (110 lbs) Zarya 1 inch 1:100 Scale A1 B1 T T T T 1 2 3 4 + PDGF EFGF TOP y R AP BKA 2AP BKA VSC L + PDGF EFGF Front R L M C C MCC FA OFB cut Aft Active hybrid docking mechanism Aft cut Passive docking mechanism (nadir) back + front + AC BKA + front inside front + of Zarya KOMPAACT 10 KOMPAACT AC BKA AC + back Front docking + KOMPAACT 11 KOMPAACT mechanism + + inside aft of Zarya cut 2ACO 1M BKA + + + 2AO BKA KA 140 + 1 2 3 back front ©2011 Not for commercial use 1 cm Print on Cardstock (90 lbs) Zarya solar panels 1 inch 1:100 Scale Folded configuration panels ©2011 Not for commercial use 1 cm Print on Cardstock (110 lbs) Zarya 1 inch inner 1:100 Scale outer outer Cut a cottonswab (37 mm of length and 2 mm of width) and inner use as a connector for the folded wing configuration outer outer inner Unity - Zarya connector ©2011 Not for commercial use 1 cm Print on Cardstock (90 lbs) 1 inch 1:100 Scale Docking Target for Zarya Module (Target used for Soyuz/Progress or MRM-1 “Rassvet”) Schematic for docking target location in Zarya: X Bottom view Left side view ©2011 Not for commercial use 1 cm Print on Cardstock (110 lbs) cut Zvezda 1 inch Zvezda aft docking cone 1:100 Scale back Regul antenna Reboost engine blocks This tube middle connector cut goes inside cut aft of Zvezda front Regul antenna 1 2 3 4 + + 5 6 7 8 9 + 10 + + 11 + K P K P 12 + + 13 14 15 16 17 18 19 20 21 22 Orange rectangle 23 is glued on top of russian flag (ISS configuration post 4R: after PIRS docking module was added to ISS) Zvezda Zvezda main large cone Zvezda body reinforcer large cone reinforcer ©2011 Not for commercial use 1 cm Print on Cardstock (110 lbs) Zvezda 1 inch 1:100 Scale + Star Mappers + + R + L + + + + + R cut + L Zvezda front docking cone + + cut + + Front Aft cut This tube goes inside Zarya - Zvezda front section of Zvezda connector ©2011 Not for commercial use Print on Cardstock (90 lbs) 1 cm Zvezda solar panels 1 inch 1:100 Scale ©2011 Not for commercial use 1 cm Print on Cardstock (110 lbs) “PIRS” Docking Module Active hybrid docking mechanism 1 inch back cut front 1:100 Scale KURS Ring 1 back KURS protection front shields AKP -BKA BA2 BA1 2ACO1-1 KURS Ring 2 EV HATCH 2 KNECT-M EV HATCH 1 2ACO1-2 2A0-BKA Ring 3 P K Ring 4 HEP I N I N HEP P K PN C PN C Ring 5 MM3-4 Ring 6 2A0-BKA CKK MM3-3 MM3-1 2A -BKA 2A 2A -BKA 2A 3 2 1 3 2 1 Docking cone cut cut ZVEZDA PIRS PIRS SOYUZ/PROGRESS ©2012 Not for commercial use 1 cm Print on Cardstock (110 lbs) MRM-2 “POISK” Active hybrid docking mechanism 1 inch back cut front 1:100 Scale KURS Ring 1 back KURS protection front shields TPAH3NT -6 EV HATCH 1 BA1 AKP -BKA AKP BA2 EV HATCH 2 HATCH EV 2ACO1-1 KURS Ring 2 KNECT-M EV HATCH 1 EV HATCH 2 2ACO1-2 2A0-BKA Ring 3 MM3-2 HEP Ring 4 I N CM ETHERNET CM I N HEP O CN K O CN K Ring 5 MM3-4 Ring 6 ETHERNET HA ETHERNET 2A0-BKA HA 2 HA KAANAM AP-2AP AP-2AP KAANAM CKK KAANAH MN EHN 3 2 1 3 2 1 Docking cone cut cut ZVEZDA POISK POISK SOYUZ/PROGRESS ©2012 Not for commercial use 1 cm Print on Cardstock (90 lbs) Mini Research Module-1 (MRM-1) 1 inch “RASSVET” 1:100 Scale Active hybrid docking mechanism Sheet 1 camera Front ON-1 ON-7 cut Ring 1 Ring 2 ON-2 TK1 521PK.000-0 AHTEHHA TBC AHTEHHA Aft ERA Elbow Spare cover A B camera ON-5 3NP 3NP ERA y A B K2 K5NPM ON-4 y K1 K K y 2-1 M01-ERA K1NPM y R Aft L 2-2 2-3 yK4NPM K2NPM y 2-4 yK4NPM yK3NPM K yK1 PTO yK2 PTO yK3 HEP HEP I N R Front L 1-1 1-2 PVGF HEP I N PACCBET M02-ERA TBC AHTEH K4 PTO K4 y y 2AP-BKA K3 PTO AP-BKA MN EHb 2 KOHTPOA R PDA 2 ON-3 4AO-BKA b MN EH CTbIKOBKN PVGF HA Trunnions (Power & Video 1 1 TK2 Grapple Fixture) cut Docking cone ©2013 Not for commercial use 1 cm Print on Cardstock (90 lbs) Mini Research Module-1 (MRM-1) 1 inch “RASSVET” 1:100 Scale Sheet 2 A A K K K IV R K Pb y ON-4 x x MN EH 77KM b0000-0 ON-29 b 2 K K K FRGF IV MLM Airlock MLM Radiator glue OTKPbITO 3TKPbITO OPEN CLOSE Portable Work Platform x x RASSVET SOYUZ ©2013 Not for commercial use 1 cm Print on Cardstock (90 lbs) 1 inch Debri Panels for smaller diameter of Zvezda 1:100 Scale (Russian EVA-31) Debri Panels installation areas 1:144 Scale ©2013 Not for commercial use.
Load more

Recommended publications
  • Moscow Defense Brief Your Professional Guide Inside # 1, 2011
    Moscow Defense Brief Your Professional Guide Inside # 1, 2011 Russian Army’s New Look CONTENTS Defense Industries #1 (23), 2011 New Management at the United Aircraft Corporation 2 PUBLISHER Centre for Analysis of Arms Trade Strategies and Russian Arms Trade in 2010 4 Technologies CAST Director & Publisher Procurement Ruslan Pukhov Editor-in-Chief Russian Military Spending in 2011-2020 12 Mikhail Barabanov Advisory Editors Konstantin Makienko Space Alexey Pokolyavin Russian Space Industry in 2010 17 Researchers Ruslan Aliev Polina Temerina Armed Forces Dmitry Vasiliev Russia’s “New-Look” Army: the Medical Service 20 Editorial Office 3 Tverskaya-Yamskaya, 24, office 5, Demographics vs the Russian Army 25 Moscow, Russia 125047 phone: +7 499 251 9069 fax: +7 495 775 0418 Our Authors 28 http://www.mdb.cast.ru/ To subscribe, contact phone: +7 499 251 9069 or e-mail: [email protected] Moscow Defense Brief is published by the Centre for Analysis of Strategies and Technologies All rights reserved. No part of this publication may be reproduced in any form or by any means, electronic, mechanical or photocopying, recording or otherwise, without reference to Moscow Defense Brief. Please note that, while the Publisher has taken all reasonable care in the compilation of this publication, the Publisher cannot accept responsibility for any errors or omissions in this publication or for any loss arising therefrom. Authors’ opinions do not necessary reflect those of the Publisher or Editor Translated by: Ivan Khokhotva Computer design & pre-press: B2B design bureau Zebra www.zebra-group.ru Cover Photo: Soldiers of the 5th Independent Motorized Rifle Brigade on a rest break during an exercise Photo by: Vadim Savitsky © Centre for Analysis of Strategies and Technologies, 2011 Printed in Russia # 1, 2011 Moscow Defense Brief 1 Defense Industries New Management at the United Aircraft Corporation Konstantin Makienko ew management has arrived at the United Aircraft Sukhoi company.
    [Show full text]
  • For Steady Production of H-II Transfer Vehicle“KOUNOTORI”Series,Mitsubishi Heavy Industries Technical Review Vol.50 No.1(20
    Mitsubishi Heavy Industries Technical Review Vol. 50 No. 1 (March 2013) 68 For Assured Production of “KOUNOTORI” Series H-II Transfer Vehicle YOICHIRO MIKI*1 KOICHI MATSUYAMA*2 KAZUMI MASUDA*3 HIROSHI SASAKI*4 The H-II Transfer Vehicle (HTV) is an unmanned but man-rated designed resupply spacecraft developed by Japan as a means of transporting supplies to the International Space Station (ISS). Since the launch of vehicle No. 1 on September 11, 2009, the HTVs have accomplished their missions three times in a row up to vehicle No. 3 in July 2012. Mitsubishi Heavy Industries, Ltd. (MHI) is managing the production of the HTVs from vehicle No. 2 as the prime contractor, and we are planning to launch another four vehicles up to No. 7. Need for the HTVs is increasing after the retirement of the U.S. Space Shuttle. This paper introduces the efforts taken for the assured production in order to maintain the continued success of the HTVs. |1. Introduction The H-II Transfer Vehicles (HTVs) have consecutively accomplished the three missions of the No. 1 demonstration flight vehicle in September 2009, the No. 2 first operational flight vehicle in January 2011 and No. 3 in July 2012. As a result of the Request for Proposal (RFP) competition, Japan Aerospace Exploration Agency (JAXA), selected Mitsubishi Heavy Industries, Ltd. (MHI) as the prime contractor for production of the operational flight HTVs as of No. 2. Accordingly, HTV No. 2 and No. 3 were manufactured under MHI’s management, leading to success. A wide variety of cargos have been transported by the three HTVs, showing the high versatility of the vehicle.
    [Show full text]
  • 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.
    [Show full text]
  • ARC-OVER April
    April Upcoming Events Next Board Meeting: May 6 Next General Meeting: May 12 Field Day: June 27 & 28 Pacificon: October 16 - 18 Dayton Hamvention May 15 TARC Meeting April 14, 2015 Turlock, War Memorial 7:00 p.m. Ron Roos, KJ6KNL, Our honorable President, called the meeting to order Pledge of Allegiance, All members and guests introduced themselves. Dylan Low, KK6SYD, was a first time guest. All were welcomed. Dick Decker, Vice President, K6SUU, gave an interesting presentation on Hams In Space. This was the topic members showed the most interest in. Fox 1 will launch on August 27th, 2015. To contact Space Stations in the past the Uplink was on VHF and the Downlink on UHF. This is now reversed, the Uplink will be UHF and the Downlink will be VHF. For a full copy of the Powerpoint Presentation, Dick announced that those interested could send an email to him and he would send it to those requesting it. Included in the Powerpoint will be the links for further information. Dick explained that Space stations were easier to use than Satellites. A variety of antennas were shown and discussed. They included; The Yagi, Two Elk Antennas (mounted on PVC) and one that really measured up; The Tape Measure Antenna. Dick informed all that he has a radio that members could use to hit the Space Station. Please contact him if you are interested. The process is pretty simple and it is rewarding when you get your card back in the mail! Dick’s email is; [email protected] 1 Ron Roos, asked members if they had read the minutes from our March 10th Meeting.
    [Show full text]
  • IAF-01-T.1.O1 Progress on the International Space Station
    https://ntrs.nasa.gov/search.jsp?R=20150020985 2019-08-31T05:38:38+00:00Z IAF-01-T.1.O1 Progress on the International Space Station - We're Part Way up the Mountain John-David F. Bartoe and Thomas Holloway NASA Johnson Space Center, Houston, Texas, USA The first phase of the International Space Station construction has been completed, and research has begun. Russian, U.S., and Canadian hardware is on orbit, ard Italian logistics modules have visited often. With the delivery of the U.S. Laboratory, Destiny, significant research capability is in place, and dozens of U.S. and Russian experiments have been conducted. Crew members have been on orbit continuously since November 2000. Several "bumps in the road" have occurred along the way, and each has been systematically overcome. Enormous amounts of hardware and software are being developed by the International Space Station partners and participants around the world and are largely on schedule for launch. Significant progress has been made in the testing of completed elements at launch sites in the United States and Kazakhstan. Over 250,000 kg of flight hardware have been delivered to the Kennedy Space Center and integrated testing of several elements wired together has progressed extremely well. Mission control centers are fully functioning in Houston, Moscow, and Canada, and operations centers Darmstadt, Tsukuba, Turino, and Huntsville will be going on line as they are required. Extensive coordination efforts continue among the space agencies of the five partners and two participants, involving 16 nations. All of them continue to face their own challenges and have achieved significant successes.
    [Show full text]
  • REV I Launch Occurred at 1:20Pm CT
    ***************************************************************************************************************************************************************************************** NASA TELEVISION SCHEDULE STS-132 ISS UTILIZATION LOGISTICS FLIGHT 4 / MINI RESEARCH MODULE 1 (RASSVET) REV I 5/24/2010 ***************************************************************************************************************************************************************************************** NASA TV (Public, Education, Media Channels and occasional HD programming) Digital Satellite C-Band Downlink coordinates for continental North America, Alaska and Hawaii: Satellite = AMC 3 / Transponder = 15C / 87 Degrees West / DVB-S, 4:2:0 / Downlink Frequency = 4000 Mhz / Downlink Polarity = Horizontal / FEC = 3/4 / Data Rate = 38.860 MHz / Symbol Rate = 28.1115. Clients actively participating in Standard-Definition on-orbit interviews, interactive press briefings and satellite interviews must use the LIMO Channel: Satellite = AMC 3 / Transponder = 9C / 87 degrees West / DVB-S, 4:2:0 / Downlink Frequency = 3865.5 Mhz / Downlink Polarity = Horizontal / FEC = 3/4 / Data Rate = 6.0 Mbps / Symbol rate = 4.3404 Msps. A Digital Video Broadcast compliant Integrated Receiver Decoder is required for reception. Mission Audio is available at: http://www.nasa.gov/ntv. ALL TIMES SUBJECT TO CHANGE This TV schedule is available via the Internet. The address is: http://www.nasa.gov/shuttletv Launch occurred at 1:20pm CT (2:20pm ET) on Friday, May 14th, 2010. An asterisk
    [Show full text]
  • 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.
    [Show full text]
  • Highlights in Space 2010
    International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no.
    [Show full text]
  • 1998 Year in Review
    Associate Administrator for Commercial Space Transportation (AST) January 1999 COMMERCIAL SPACE TRANSPORTATION: 1998 YEAR IN REVIEW Cover Photo Credits (from left): International Launch Services (1998). Image is of the Atlas 2AS launch on June 18, 1998, from Cape Canaveral Air Station. It successfully orbited the Intelsat 805 communications satellite for Intelsat. Boeing Corporation (1998). Image is of the Delta 2 7920 launch on September 8, 1998, from Vandenberg Air Force Base. It successfully orbited five Iridium communications satellites for Iridium LLP. Lockheed Martin Corporation (1998). Image is of the Athena 2 awaiting its maiden launch on January 6, 1998, from Spaceport Florida. It successfully deployed the NASA Lunar Prospector. Orbital Sciences Corporation (1998). Image is of the Taurus 1 launch from Vandenberg Air Force Base on February 10, 1998. It successfully orbited the Geosat Follow-On 1 military remote sensing satellite for the Department of Defense, two Orbcomm satellites and the Celestis 2 funerary payload for Celestis Corporation. Orbital Sciences Corporation (1998). Image is of the Pegasus XL launch on December 5, 1998, from Vandenberg Air Force Base. It successfully orbited the Sub-millimeter Wave Astronomy Satellite for the Smithsonian Astrophysical Observatory. 1998 YEAR IN REVIEW INTRODUCTION INTRODUCTION In 1998, U.S. launch service providers conducted In addition, 1998 saw continuing demand for 22 launches licensed by the Federal Aviation launches to deploy the world’s first low Earth Administration (FAA), an increase of 29 percent orbit (LEO) communication systems. In 1998, over the 17 launches conducted in 1997. Of there were 17 commercial launches to LEO, 14 these 22, 17 were for commercial or international of which were for the Iridium, Globalstar, and customers, resulting in a 47 percent share of the Orbcomm LEO communications constellations.
    [Show full text]
  • Post Increment Evaluation Report Increment 11 International Space
    SSP 54311 Baseline WWW.NASAWATCH.COM Post Increment Evaluation Report Increment 11 International Space Station Program Baseline June 2006 National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract Number: NNJ04AA02C WWW.NASAWATCH.COM SSP 54311 Baseline - WWW.NASAWATCH.COM REVISION AND HISTORY PAGE REV. DESCRIPTION PUB. DATE - Initial Release (Reference per SSCD XXXXXX, EFF. XX-XX-XX) XX-XX-XX WWW.NASAWATCH.COM SSP 54311 Baseline - WWW.NASAWATCH.COM INTERNATIONAL SPACE STATION PROGRAM POST INCREMENT EVALUATION REPORT INCREMENT 11 CHANGE SHEET Month XX, XXXX Baseline Space Station Control Board Directive XXXXXX/(X-X), dated XX-XX-XX. (X) CHANGE INSTRUCTIONS SSP 54311, Post Increment Evaluation Report Increment 11, has been baselined by the authority of SSCD XXXXXX. All future updates to this document will be identified on this change sheet. WWW.NASAWATCH.COM SSP 54311 Baseline - WWW.NASAWATCH.COM INTERNATIONAL SPACE STATION PROGRAM POST INCREMENT EVALUATION REPORT INCREMENT 11 Baseline (Reference SSCD XXXXXX, dated XX-XX-XX) LIST OF EFFECTIVE PAGES Month XX, XXXX The current status of all pages in this document is as shown below: Page Change No. SSCD No. Date i - ix Baseline XXXXXX Month XX, XXXX 1-1 Baseline XXXXXX Month XX, XXXX 2-1 - 2-2 Baseline XXXXXX Month XX, XXXX 3-1 - 3-3 Baseline XXXXXX Month XX, XXXX 4-1 - 4-15 Baseline XXXXXX Month XX, XXXX 5-1 - 5-10 Baseline XXXXXX Month XX, XXXX 6-1 - 6-4 Baseline XXXXXX Month XX, XXXX 7-1 - 7-61 Baseline XXXXXX Month XX, XXXX A-1 - A-9 Baseline XXXXXX Month XX, XXXX B-1 - B-3 Baseline XXXXXX Month XX, XXXX C-1 - C-2 Baseline XXXXXX Month XX, XXXX D-1 - D-92 Baseline XXXXXX Month XX, XXXX WWW.NASAWATCH.COM SSP 54311 Baseline - WWW.NASAWATCH.COM INTERNATIONAL SPACE STATION PROGRAM POST INCREMENT EVALUATION REPORT INCREMENT 11 JUNE 2006 i SSP 54311 Baseline - WWW.NASAWATCH.COM SSCB APPROVAL NOTICE INTERNATIONAL SPACE STATION PROGRAM POST INCREMENT EVALUATION REPORT INCREMENT 11 JUNE 2006 Michael T.
    [Show full text]
  • 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.
    [Show full text]
  • Space Policies, Issues and Trends in 2010/2011
    Space Policies, Issues and Trends in 2010/2011 Report 35 June 2011 Spyros Pagkratis Short title: ESPI Report 35 ISSN: 2076-6688 Published in June 2011 Price: €11 Editor and publisher: European Space Policy Institute, ESPI Schwarzenbergplatz 6 • 1030 Vienna • Austria http://www.espi.or.at Tel. +43 1 7181118-0; Fax -99 Rights reserved – No part of this report may be reproduced or transmitted in any form or for any purpose with- out permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “Source: ESPI Report 35; June 2011. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, inciden- tal or consequential, resulting from the information contained in this publication. Design: Panthera.cc ESPI Report 35 2 June 2011 Space Policies, Issues and Trends in 2010/2011 Table of Contents 1. Global Political and Economic Trends 5 1.1 Global Economic Outlook 5 1.2 Political Developments 6 1.2.1 Security 6 1.2.2 Environment 7 1.2.3 Energy 7 1.2.4 Resources 8 1.2.5 Knowledge 8 1.2.6 Mobility 11 2. Global Space Sector Size and Developments 12 2.1 Global Space Budgets and Revenues 12 2.2 Overview of Institutional Space Budgets 12 2.3 Overview of Commercial Space Markets 16 2.3.1 Satellite Services 16 2.3.2 Satellite Manufacturing 19 2.3.3 Launch Sector 19 2.3.4.
    [Show full text]