Successful Mission of Tupod, an Innovative Cubesat, a Tubesats Deployer Manufactured Via Additive Manufacturing by CRP USA Using Windform® XT 2.0 Composite Material
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Tupod Press Release
G.A.U.S.S. SRL Via Lariana 5, Rome – Italy Phone: +39 06 97881440 GROUP OF ASTRODYNAMICS VAT No.: IT11900481000 FOR THE USE OF [email protected] SPACE SYSTEMS www.gaussteam.com TuPOD is ready for launch – Press Release – 5 December 2016 The TuPOD, a 3U CubeSat satellite and at the same time a deployer of TubeSat (a type of small satellite), originates from an innovative project of the Company G.A.U.S.S. Srl (Group of Astrodynamics for the Use of Space Systems), specialized in the development of satellites that are launcher platforms as well (like the previous satellites UniSat-5 and UniSat-6). The TuPOD is a CubeSat-type of satellite, with dimensions of 10x10x30cm, which will work itself as launch system for smaller satellites, the TubeSats. The TubeSats are a new type of Nanosatellites, cylindrically-shaped, not much bigger than an ordinary beverage can. To date, there wasn’t any launch possibility for this class of small satellites: with the TuPOD project, GAUSS Srl creates a new and affordable launch opportunity for the users of this new type of satellite. The TuPOD hosts two TubeSats onboard: TANCREDO I (Brazil) and OSNSAT (USA). Thanks to this specific kind of deployer – designed and built by GAUSS Srl – a couple of TubeSats are about to be UniSat-6 Platform released into Space for the first time ever. An important milestone for GAUSS Srl and for the whole Italian Aerospace Community. The TuPOD, in the middle, satellite/deployer for TubeSats from GAUSS Srl. On the right and on the left the TubeSats OSNSAT and TANCREDO I. -
Launch / Tracking and Control Plan of Advanced Land Observing Satellite (ALOS) / H-IIA Launch Vehicle No
Launch / Tracking and Control Plan of Advanced Land Observing Satellite (ALOS) / H-IIA Launch Vehicle No. 8 (H-IIA F8) November 2005 Japan Aerospace Exploration Agency (JAXA) (Independent Administrative Agency) - 1 - Table of Contents Page 1. Overview of the Launch / Tracking and Control Plan 1 1.1 Organization in Charge of Launch / Tracking and Control 1 1.2 Person in Charge of Launch / Tracking and Control Operations 1 1.3 Objectives of Launch / Tracking and Control 1 1.4 Payload and Launch Vehicle 1 1.5 Launch Window (Day and Time) 2 1.6 Facilities for Launch / Tracking and Control 2 2. Launch Plan 3 2.1 Launch Site 3 2.2 Launch Organization 4 2.3 Launch Vehicle Flight Plan 5 2.4 Major Characteristics of the Launch Vehicle 5 2.5 Outline of the Advanced Land Observing Satellite (ALOS) 5 2.6 Securing Launch Safety 5 2.7 Correspondence Method of Launch information to Parties Concerned 6 3. Tracking and Control Plan 8 3.1 Tracking and Control Plan of the ALOS 8 3.1.1 Tracking and Control Sites 8 3.1.2 Tracking and Control Organization 8 3.1.3 Tracking and Control Period 8 3.1.4 Tracking and Control Operations 10 3.1.5 ALOS Flight Plan 10 3.1.6 Tracking and Control System 10 4. Launch Result Report 11 [List of Tables] Table-1: Launch Vehicle Flight Plan 13 Table-2: Major Characteristics of the Launch Vehicle 15 Table-3: Major Characteristics of the ALOS 17 Table-4: Tracking and Control Plan (Stations) of the ALOS 23 [List of Figures] Figure-1: Map of Launch / Tracking and Control Facilities 12 Figure-2: Launch Vehicle Flight Trajectory 14 Figure-3: Configuration of the Launch Vehicle 16 Figure-4: On-orbit Configuration of the ALOS 20 Figure-5: Access Control Areas for Launch 21 Figure-6: Impact Areas of the Launch Vehicle 22 Figure-7: ALOS Flight Plan 24 Figure-8: ALOS Footprint 25 Figure-9: ALOS Tracking and Control System 26 - 2 - 1. -
X103 H-IIB Launch Vehicle H-IIBロケット
Outdoor Exhibition Outdoor X103 H-IIB Launch Vehicle H-IIBロケット ■Purpose of Exhibition The domestically produced large rocket "H-IIB" is exhibited in the outdoor exhibition space. Most of this rocket has the same structure as the real rocket and served as a test. You can find the real parts in the chart including the first stage engine section, the first stage fuel tank, the center body section, the interstage adapter and the fairing, which are exhibited in the exhibition. The rest of the parts were made by referring to the actual rocket. When the rocket "H-IIB" is launched, two other main engines and four fixed rocket boosters are attached to the rocket. You can see the inside structure because the tank part is cut off. For making a light but strong rocket, it is manufactured like a honeycomb. For pouring low temperature liquid- hydrogen into the tank, the exterior of the rocket is coated by a thermal material. The rocket which is exhibited is also coated by using the same thermal material. Like this, the rockets were made by using the latest manufacturing technology and design techniques. We would like you to learn the structure of rocket and feel how big it is. ■Additional Knowledge Space Station had succeeded. The Japanese high- launching technology which put the rocket into the planned orbit accurately, and the connecting technology which controlled the HTV delicately and connected to the International Space Station in outer space, has been shown to the world. [The Other Rockets Exhibition in Japan] There are rocket exhibitions in regions where JAXA developed space technology (as of 2010).The Tanegashima Space Center is where the JAXA Research Institute is located in Tanegashima, Kagoshima Prefecture. -
Securing Japan an Assessment of Japan´S Strategy for Space
Full Report Securing Japan An assessment of Japan´s strategy for space Report: Title: “ESPI Report 74 - Securing Japan - Full Report” Published: July 2020 ISSN: 2218-0931 (print) • 2076-6688 (online) Editor and publisher: European Space Policy Institute (ESPI) Schwarzenbergplatz 6 • 1030 Vienna • Austria Phone: +43 1 718 11 18 -0 E-Mail: [email protected] Website: www.espi.or.at Rights reserved - No part of this report may be reproduced or transmitted in any form or for any purpose without permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “ESPI Report 74 - Securing Japan - Full Report, July 2020. 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, incidental or consequential, resulting from the information contained in this publication. Design: copylot.at Cover page picture credit: European Space Agency (ESA) TABLE OF CONTENT 1 INTRODUCTION ............................................................................................................................. 1 1.1 Background and rationales ............................................................................................................. 1 1.2 Objectives of the Study ................................................................................................................... 2 1.3 Methodology -
January 2017 AEROSPACE
AEROSPACE January 2017 44 Number 1 Volume Society Royal Aeronautical JANUARY 2017 NEWSPACE START- UPS AIM FOR ORBIT BREXIT – TAILWIND OR TURBULENCE? VIRTUAL HELICOPTER DESIGN www.aerosociety.com REDRESSING THE BALANCE RECRUITING MORE FEMALE PILOTS Have you renewed your Membership Subscription for 2017? Your membership subscription is due on 1 January 2017 and any unpaid memberships will lapse on 31 March 2017. As per the Society’s Regulations, all How to renew: membership benefits will be suspended where Online: a payment for an individual subscription has Log in to your account on the Society’s www.aerosociety.com not been received after three months of the website to pay at . If you due date. However, this excludes members do not have an account, you can register online paying their annual subscriptions by Direct and pay your subscription straight away. Debits in monthly instalments to October. Telephone: Call the Subscriptions Department +44 (0)20 7670 4315 / 4304 We don’t want you to lose all of your on membership benefits, which include: Cheque: Cheques should be made payable to • Your monthly subscription to AEROSPACE the Royal Aeronautical Society and sent to the magazine Subscriptions Department at No.4 Hamilton • Use of your RAeS post nominals as Place, London W1J 7BQͭ UK. applicable Direct Debit: Complete the Direct Debit • Over 400 global events yearly mandate form included in your renewal letter • Discounted rates for conferences or complete the mandate form online once you • Online publications including Society News, have logged into your account by 16 January. blogs and podcasts BACS Transfer: • Involvement with your local branch Pay by Bank Transfer (or by • Networking opportunities BACS) into the Society’s bank account, quoting your name and membership number. -
Japan's Technical Prowess International Cooperation
Japan Aerospace Exploration Agency April 2016 No. 10 Special Features Japan’s Technical Prowess Technical excellence and team spirit are manifested in such activities as the space station capture of the HTV5 spacecraft, development of the H3 Launch Vehicle, and reduction of sonic boom in supersonic transport International Cooperation JAXA plays a central role in international society and contributes through diverse joint programs, including planetary exploration, and the utilization of Earth observation satellites in the environmental and disaster management fields Japan’s Technical Prowess Contents No. 10 Japan Aerospace Exploration Agency Special Feature 1: Japan’s Technical Prowess 1−3 Welcome to JAXA TODAY Activities of “Team Japan” Connecting the Earth and Space The Japan Aerospace Exploration Agency (JAXA) is positioned as We review some of the activities of “Team the pivotal organization supporting the Japanese government’s Japan,” including the successful capture of H-II Transfer Vehicle 5 (HTV5), which brought overall space development and utilization program with world- together JAXA, NASA and the International Space Station (ISS). leading technology. JAXA undertakes a full spectrum of activities, from basic research through development and utilization. 4–7 In 2013, to coincide with the 10th anniversary of its estab- 2020: The H3 Launch Vehicle Vision JAXA is currently pursuing the development lishment, JAXA defined its management philosophy as “utilizing of the H3 Launch Vehicle, which is expected space and the sky to achieve a safe and affluent society” and to become the backbone of Japan’s space development program and build strong adopted the new corporate slogan “Explore to Realize.” Under- international competitiveness. -
Hazard Analysis of Complex Spacecraft Using Systems- Theoretic Process Analysis *
Hazard Analysis of Complex Spacecraft using Systems- Theoretic Process Analysis * Takuto Ishimatsu†, Nancy G. Leveson‡, John P. Thomas§, and Cody H. Fleming¶ Massachusetts Institute of Technology, Cambridge, Massachusetts 02139 Masafumi Katahira#, Yuko Miyamoto**, and Ryo Ujiie†† Japan Aerospace Exploration Agency, Tsukuba, Ibaraki 305-8505, Japan Haruka Nakao‡‡ and Nobuyuki Hoshino§§ Japan Manned Space Systems Corporation, Tsuchiura, Ibaraki 300-0033, Japan Abstract A new hazard analysis technique, called System-Theoretic Process Analysis, is capable of identifying potential hazardous design flaws, including software and system design errors and unsafe interactions among multiple system components. Detailed procedures for performing the hazard analysis were developed and the feasibility and utility of using it on complex systems was demonstrated by applying it to the Japanese Aerospace Exploration Agency H-II Transfer Vehicle. In a comparison of the results of this new hazard analysis technique to those of the standard fault tree analysis used in the design and certification of the H-II Transfer Vehicle, System-Theoretic Hazard Analysis found all the hazardous scenarios identified in the fault tree analysis as well as additional causal factors that had not been) identified by fault tree analysis. I. Introduction Spacecraft losses are increasing stemming from subtle and complex interactions among system components. The loss of the Mars Polar Lander is an example [1]. The problems arise primarily because the growing use of software allows engineers to build systems with a level of complexity that precludes exhaustive testing and thus assurance of the removal of all design errors prior to operational use [2,3] Fault Tree Analysis (FTA) and Failure Modes and Effects Analysis (FMEA) were created long ago to analyze primarily electro-mechanical systems and identify potential losses due to component failure. -
DECEMBER CURRENT AFFAIRS 2016 Appointed Former Sebi Chief C B Bhave As Nonexecutive Chairman and Independent Director
COMPLETE SUCCESS BANK PO/CLERICAL COACHING DECEMBER CURRENT AFFAIRS 2016 appointed former Sebi chief C B Bhave as nonexecutive Chairman and Independent Director. Appointments 29. Maha Vajiralongkorn became King of Thailand, after his 1. A. K. Dhasmana is appointed as new Chief of Research& Father Bhumibol Adulyadej died (Follwoing a record 70 years Analysis Wing (RAW). Rajiv Jain is appointed as chief of reign). Intelligence Bureau. 30. Mian Saqib Nisar appointed as 25th Chief Justice of Pakistan. 2. Actor Salman Khan named as ambassador of Brihan-mumbai 31. Nana AkufoAddo won presidential election of Ghana (West Municipal Corporation' drive against open defecation and litter Africa). under Swatch Bharat Mission. 32. National Party’s Bill English has been appointed as new (39th) 3. Actress Priyanka Chopra named as brand ambassador for Prime Minister of New Zealand Assam tourism. 33. Naveed Mukhtar is appointed as new chief of Pakistan’s spy 4. Adwaita Gadanayak has been appointed as Director General of agency Inter-Services Intelligence (ISI). National Gallery of Modern Art (NGMA). 34. Navy Chief Sunil Lanba is appointed as Chairman of the Chiefs 5. Air Marshal Birender Singh Dhanoa will be new Chief of Indian of Staff committee (COSC). Air Force, on retirement of Current IAF Chief Arup Raha. 35. Nigeria’s Environment Minister Amina Mohammed appointed 6. Airline AirAsia India appointed Amar Abrol as Managing as Deputy Secretary-General of United Nations. Director. 36. P R Sreejesh appointed as Goalkeeping coach of Under 21 7. Akbar Ebrahim elected as president of Chennai based Hockey Team. Federation of Motor Sports Clubs of India (FMSCI). -
H-2 Family Home Launch Vehicles Japan
Please make a donation to support Gunter's Space Page. Thank you very much for visiting Gunter's Space Page. I hope that this site is useful a nd informative for you. If you appreciate the information provided on this site, please consider supporting my work by making a simp le and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much. H-2 Family Home Launch Vehicles Japan H-2 (ETS 6) [NASDA] H-2 with SSB (SFU / GMS 5) [NASDA] H-2S (MTSat 1) [NASDA] H-2A-202 (GPM) [JAXA] 4S fairing H-2A-2022 (SELENE) [JAXA] H-2A-2024 (MDS 1 / VEP 3) [NASDA] H-2A-204 (ETS 8) [JAXA] H-2B (HTV 3) [JAXA] Version Strap-On Stage 1 Stage 2 H-2 (2 × SRB) 2 × SRB LE-7 LE-5A H-2 (2 × SRB, 2 × SSB) 2 × SRB LE-7 LE-5A 2 × SSB H-2S (2 × SRB) 2 × SRB LE-7 LE-5B H-2A-1024 * 2 × SRB-A LE-7A - 4 × Castor-4AXL H-2A-202 2 × SRB-A LE-7A LE-5B H-2A-2022 2 × SRB-A LE-7A LE-5B 2 × Castor-4AXL H-2A-2024 2 × SRB-A LE-7A LE-5B 4 × Castor-4AXL H-2A-204 4 × SRB-A LE-7A LE-5B H-2A-212 ** 1 LRB / 2 LE-7A LE-7A LE-5B 2 × SRB-A H-2A-222 ** 2 LRB / 2 × 2 LE-7A LE-7A LE-5B 2 × SRB-A H-2A-204A ** 4 × SRB-A LE-7A Widebody / LE-5B H-2A-222A ** 2 LRB / 2 × LE-7A LE-7A Widebody / LE-5B 2 × SRB-A H-2B-304 4 × SRB-A Widebody / 2 LE-7A LE-5B H-2B-304A ** 4 × SRB-A Widebody / 2 LE-7A Widebody / LE-5B * = suborbital ** = under stud y Performance (kg) LEO LPEO SSO GTO GEO MolO IP H-2 (2 × SRB) 3800 H-2 (2 × SRB, 2 × SSB) 3930 H-2S (2 × SRB) 4000 H-2A-1024 - - - - - - - H-2A-202 10000 4100 H-2A-2022 4500 H-2A-2024 5000 H-2A-204 6000 H-2A-212 -
HTV-1 Mission Press Kit
HTV-1 Mission Press Kit September 9, 2009 Rev.A Japan Aerospace Exploration Agency Revision History No. Date Page revised Reason for the revision NC 2009.9.2 - A 2009.9.9 P.2-2, P.2-3, ・ Launch time was rescheduled P.2-9 to P.2-16 ・ HTV’s flight timeline was changed P.2-23 to P.2-25 ・ Small changes in descriptions of SMILES and HREP Contents 1. H-II Transfer Vehicle Overview............................................................................1-1 1.1 Summary ..........................................................................................................1-1 1.1.1 Objectives and Significance.................................................................... 1-2 1.1.2 Features................................................................................................... 1-2 1.2 HTV Component..............................................................................................1-4 1.2.1 Pressurized Logistic Carrier (PLC)........................................................ 1-7 1.2.2 Unpressurized Logistic Carrier (ULC)................................................. 1-11 1.2.3 Exposed Pallet (EP) .............................................................................. 1-13 1.2.4 Avionics Module.................................................................................... 1-16 1.2.5 Propulsion Module................................................................................ 1-19 1.2.6 Proximity Communication System (PROX)....................................... 1-21 1.2.7 Laser Rader Reflector -
Modelling the ISS
Spaceflight A British Interplanetary Society Publication Modelling the ISS Hermes at 25 Cape pads Vol 59 No 4 April 2017 £4.50 www.bis-space.com CONTENTS Editor: Published by the British Interplanetary Society David Baker, PhD, BSc, FBIS, FRHS Sub-editor: Volume 59 No. 4 April 2017 Ann Page Production Assistant: Ben Jones 130-133 The birth of Cape Canaveral Joel W. Powell has long had an interest in the origins and development Spaceflight Promotion: Gillian Norman of the Cape Canaveral facilities and again shares with us another chapter in the history of this remarkable place, from where the first US Spaceflight Arthur C. Clarke House, satellites were launched and from where early rocket tests took place. 27/29 South Lambeth Road, London, SW8 1SZ, England. 134-143 Modelling the ISS Tel: +44 (0)20 7735 3160 Keith McNeill shares with us his extraordinary effort at building a model Fax: +44 (0)20 7582 7167 of the International Space Station. Combined with masterful skills at Email: [email protected] making miniature modules and trusses, Keith brings great talent to bear www.bis-space.com with his photographic expertise. ADVERTISING 144-149 ESA’s spaceplane at T+25 years Tel: +44 (0)1424 883401 Email: [email protected] Luc van den Abeelen looks back to European aspirations for an autonomous spaceplane capable of carrying astronauts into space DISTRIBUTION Spaceflight may be received worldwide by and conducting research experiments in microgravity conditions, re- mail through membership of the British examining the Hermes programme and its many vicissitudes. Interplanetary Society. -
Business Partnership and Technology Transfer Opportunities in the Space
EU-Japan Centre for Industrial Cooperation 日欧産業協力センター The Space Sector EU- Japan business and technological cooperation potential Veronica La Regina Minerva Fellow Tokyo 2015 1 Abstract This report aims to propose the best way of pursuing the EU-Japan industrial cooperation in the field of Space. Firstly, it reviews European and Japanese current cooperation in the field of Space. Secondly, it investigates the current level of trade between the two partners in order to understand the best way to generate further cooperation. Thirdly, the Report hopes to inform both sides about each region’s current Space sector landscape from the political, policy and industrial point of views. Fourthly, it identifies areas of industrial cooperation for which local gaps in knowledge or experience could be filled by foreign expertise, for example the European technological gaps in the small-size satellite constellation could be filled by the Japanese expertise while the Japanese intention to become more commercially oriented could be supported by the more expansive European experience in this area. Finally, recommendations to the Japanese and European stakeholders are provided. Disclaimer & Copyright Notice The information contained herein reflects the views of the author, and not necessarily the views of the EU- Japan Centre for Industrial Cooperation or the views of the EU Commission or Japanese institutions. While utmost care was taken in the preparation of the report, the author and the EU-Japan Centre cannot be held responsible for any errors. This report does not constitute legal advice in terms of business development cases. The author can be reached at [email protected] © EU-Japan Centre for industrial Cooperation 2 Acknowledgement Though only my name appears on the cover of this report, a great many people have contributed to it.