Semi- Annual Launch Report Second Half of 2009
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NASA's Lunar Atmosphere and Dust Environment Explorer (LADEE)
Geophysical Research Abstracts Vol. 13, EGU2011-5107-2, 2011 EGU General Assembly 2011 © Author(s) 2011 NASA’s Lunar Atmosphere and Dust Environment Explorer (LADEE) Richard Elphic (1), Gregory Delory (1,2), Anthony Colaprete (1), Mihaly Horanyi (3), Paul Mahaffy (4), Butler Hine (1), Steven McClard (5), Joan Salute (6), Edwin Grayzeck (6), and Don Boroson (7) (1) NASA Ames Research Center, Moffett Field, CA USA ([email protected]), (2) Space Sciences Laboratory, University of California, Berkeley, CA USA, (3) Laboratory for Atmospheric and Space Physics, University of Colorado, Boulder, CO USA, (4) NASA Goddard Space Flight Center, Greenbelt, MD USA, (5) LunarQuest Program Office, NASA Marshall Space Flight Center, Huntsville, AL USA, (6) Planetary Science Division, Science Mission Directorate, NASA, Washington, DC USA, (7) Lincoln Laboratory, Massachusetts Institute of Technology, Lexington MA USA Nearly 40 years have passed since the last Apollo missions investigated the mysteries of the lunar atmosphere and the question of levitated lunar dust. The most important questions remain: what is the composition, structure and variability of the tenuous lunar exosphere? What are its origins, transport mechanisms, and loss processes? Is lofted lunar dust the cause of the horizon glow observed by the Surveyor missions and Apollo astronauts? How does such levitated dust arise and move, what is its density, and what is its ultimate fate? The US National Academy of Sciences/National Research Council decadal surveys and the recent “Scientific Context for Exploration of the Moon” (SCEM) reports have identified studies of the pristine state of the lunar atmosphere and dust environment as among the leading priorities for future lunar science missions. -
LCROSS (Lunar Crater Observation and Sensing Satellite) Observation Campaign: Strategies, Implementation, and Lessons Learned
Space Sci Rev DOI 10.1007/s11214-011-9759-y LCROSS (Lunar Crater Observation and Sensing Satellite) Observation Campaign: Strategies, Implementation, and Lessons Learned Jennifer L. Heldmann · Anthony Colaprete · Diane H. Wooden · Robert F. Ackermann · David D. Acton · Peter R. Backus · Vanessa Bailey · Jesse G. Ball · William C. Barott · Samantha K. Blair · Marc W. Buie · Shawn Callahan · Nancy J. Chanover · Young-Jun Choi · Al Conrad · Dolores M. Coulson · Kirk B. Crawford · Russell DeHart · Imke de Pater · Michael Disanti · James R. Forster · Reiko Furusho · Tetsuharu Fuse · Tom Geballe · J. Duane Gibson · David Goldstein · Stephen A. Gregory · David J. Gutierrez · Ryan T. Hamilton · Taiga Hamura · David E. Harker · Gerry R. Harp · Junichi Haruyama · Morag Hastie · Yutaka Hayano · Phillip Hinz · Peng K. Hong · Steven P. James · Toshihiko Kadono · Hideyo Kawakita · Michael S. Kelley · Daryl L. Kim · Kosuke Kurosawa · Duk-Hang Lee · Michael Long · Paul G. Lucey · Keith Marach · Anthony C. Matulonis · Richard M. McDermid · Russet McMillan · Charles Miller · Hong-Kyu Moon · Ryosuke Nakamura · Hirotomo Noda · Natsuko Okamura · Lawrence Ong · Dallan Porter · Jeffery J. Puschell · John T. Rayner · J. Jedadiah Rembold · Katherine C. Roth · Richard J. Rudy · Ray W. Russell · Eileen V. Ryan · William H. Ryan · Tomohiko Sekiguchi · Yasuhito Sekine · Mark A. Skinner · Mitsuru Sôma · Andrew W. Stephens · Alex Storrs · Robert M. Suggs · Seiji Sugita · Eon-Chang Sung · Naruhisa Takatoh · Jill C. Tarter · Scott M. Taylor · Hiroshi Terada · Chadwick J. Trujillo · Vidhya Vaitheeswaran · Faith Vilas · Brian D. Walls · Jun-ihi Watanabe · William J. Welch · Charles E. Woodward · Hong-Suh Yim · Eliot F. Young Received: 9 October 2010 / Accepted: 8 February 2011 © The Author(s) 2011. -
G. Madhavan Nair - Wikipedia, the Free Encyclopedia
G. Madhavan Nair - Wikipedia, the free encyclopedia G. Madhavan Nair From Wikipedia, the free encyclopedia G. Madhavan Nair (Malayalam: ജി. മാധവ നായ) (born October 31, 1943) is the G Madhavan Nair present Chairman of Indian Space Research Organisation and Secretary to the Department of Space, Government of India since September 2003. He is also the Chairman, Space Commission and acts as the Chairman of Governing Body of the Antrix Corporation, Bangalore. Madhavan Nair was awarded the Padma Vibhushan, India's second highest civilian honour, on January 26, 2009.[1][2] Contents 1 Early life 2 Career 3 As Chairman of ISRO 4 Additional responsibilities G Madhavan Nair 5 Awards Born 31 October 1943 6 Honours Thiruvanathapuram, India 7 Fellowships/Memberships 8 Lashkar Threat Residence India 9 References Nationality Indian 10 External links Fields Rocket Technology Institutions Indian Space Research Organisation Bhabha Atomic Research Center Early life Alma mate r B.Sc. (Engineering - Electrical & Communication) (1966), College of Nair was born at Neyyattinkara near Thiruvananthapuram, Kerala, India. He also studied in his Engineering, Trivandrum early life in Kanyakumari District. He graduated with a B.Sc. in Engineering (1966) from College Known for Indian Space Program of Engineering, Thiruvananthapuram, Kerala University with specialization in Electrical & Communication Engineering. After his graduation Nair attended a training program at the Bhabha Notable Padma Bhushan (1998) awards Atomic Research Center (BARC) Training School, Mumbai. Padma Vibhushan (2009) Career Nair is a leading technologist in the field of rocket systems and has made significant contribution to the development of multi-stage satellite launch vehicles, achieving self-reliance in independent access to space using indigenous technologies. -
3640 H 28066 Mpeg2/Fta (Gak Di Acak) Ariana National Satelit
Thaicom 5/6A at 78.5°E (Arah Barat dari Palapa D) 3640 H 28066 Mpeg2/Fta (gak di acak) Ariana National Satelit: Insat 3a (93,5 BT) 4141 V 5150 (C Band) Mpeg2/Fta Beam menjangkau seluruh Indonesia Ke arah barat dari Palapa D, sebelum Measat 3 Telkom 1 (108,5 °E) 3776 H 4280 MPEG2/FTA/BISS HeilongjiangTV (Full Match) Chinasat 6A (125 BT) - Arah Timur dari Palapa D dan Chinasat 6B 3983 H 6880 MPEG2/FTA XJTV5 (Full Match) Chinasat 6A (125 BT) - Arah Timur dari Palapa D dan Chinasat 6B 4121 H 27500 MPEG2/FTA CCTV1 dengan frekuensi : 03840 SymbolRate: 27500 polaritas : H CCTV1 dengan frekuensi 3840 SR 27500 pol H akan menyiarkan bergantian dengan CCT V7 ( frekuensi sama) ?#?SATELIT? & CHANNEL Satelit: ST 2 (88.0°E) ID: SCC TV3 (Iran) 3587 H 12500 (C Band) 11050 V 30000 (Ku Band) MPEG4/SD/BISS SID: 0103/0068 KEY: 1111 1111 1111 1111 Satelit: ST 2 (88.0°E) ID: SCC Varzesh (Ku Band) (Iran) 11050 V 30000 MPEG4/SD/BISS SID: 0116/0117/0075 KEY: 1111 1111 1111 11i11 Satelit: Telkom 1 (108 BT) RTTL (Timor Leste) 3775 H 4280 (C Band) MPEG2/SD/FTA/BISS Satelit: Measat 3 (91,5 BT) TV1 (Malaysia) 3918 H 18385 MPEG4/SD/HD/FTA Satelit: Insat 3a (93,5 BT) Ariana (Afghanistan) 4141 V 5151 (C Band) MPEG2/SD/FTA Satelit: Chinasat 6b (115,5 BT) CCTV 1 (China) 3840 H 27500 (C Band) MPEG2/SD/FTA Satelit: Chinasat 6a (125 BT) CCTV 1 (China) 4080 H 27500 (C Band) MPEG2/SD/FTA Satelit: Chinasat 6a (125 BT) XJTV 5 (China) 4120 H 27500 (C Band) MPEG2/SD/FTA Satelit: Optus D1 (160.0°E) ID: SBS One HD 12390 H 12600 (Ku Band) (MPEG4/HD/FTA) Satelit: Thaicom5 (78,5 BT) CH8 SD, CH8 HD (Thailand) 3800 H 30000 MPEG2/SD/BISS(CH8 HD, Mpeg4/HD/BISS Satelit: Thaicom5 (78,5 BT) BBTV Ch 7 SD, BBTV Ch 7 HD (Thailand) -BBTV Ch 7 SD 3725 H 4700 -BBTV Ch 7 HD 3835 H 8000 MPEG4/HD/BISS 1. -
Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports
Commercial Space Transportation 2006 Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports January 2006 HQ003606.INDD 2006 U.S. Commercial Space Transportation Developments and Concepts About FAA/AST About the 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 49 United States Code, Subtitle IX, Chapter 701 (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 encour- age, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA/AST’s web site at http://ast.faa.gov. Federal Aviation Administration Office of Commercial Space Transportation i About FAA/AST 2006 U.S. Commercial Space Transportation Developments and Concepts 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 Federal Aviation Administration Office of Commercial Space Transportation 2006 U.S. Commercial Space Transportation Developments and Concepts Contents Table of Contents Introduction . .1 Significant 2005 Events . .4 Space Competitions . .6 Expendable Launch Vehicles . .9 Current Expendable Launch Vehicle Systems . .9 Atlas 5 - Lockheed Martin Corporation . -
Annual Report 2017 - 2018 Annual Report 2017 - 2018 Citizens’ Charter of Department of Space
GSAT-17 Satellites Images icro M sat ries Satellit Se e -2 at s to r a C 0 SAT-1 4 G 9 -C V L S P III-D1 -Mk LV GS INS -1 C Asia Satell uth ite o (G S S A T - 09 9 LV-F ) GS ries Sat Se ellit t-2 e sa to 8 r -C3 a LV C PS Annual Report 2017 - 2018 Annual Report 2017 - 2018 Citizens’ Charter of Department Of Space Department Of Space (DOS) has the primary responsibility of promoting the development of space science, technology and applications towards achieving self-reliance and facilitating in all round development of the nation. With this basic objective, DOS has evolved the following programmes: • Indian National Satellite (INSAT) programme for telecommunication, television broadcasting, meteorology, developmental education, societal applications such as telemedicine, tele-education, tele-advisories and similar such services • Indian Remote Sensing (IRS) satellite programme for the management of natural resources and various developmental projects across the country using space based imagery • Indigenous capability for the design and development of satellite and associated technologies for communications, navigation, remote sensing and space sciences • Design and development of launch vehicles for access to space and orbiting INSAT / GSAT, IRS and IRNSS satellites and space science missions • Research and development in space sciences and technologies as well as application programmes for national development The Department Of Space is committed to: • Carrying out research and development in satellite and launch vehicle technology with a goal to achieve total self reliance • Provide national space infrastructure for telecommunications and broadcasting needs of the country • Provide satellite services required for weather forecasting, monitoring, etc. -
Atlas V Cutaway Poster
ATLAS V Since 2002, Atlas V rockets have delivered vital national security, science and exploration, and commercial missions for customers across the globe including the U.S. Air Force, the National Reconnaissance Oice and NASA. 225 ft The spacecraft is encapsulated in either a 5-m (17.8-ft) or a 4-m (13.8-ft) diameter payload fairing (PLF). The 4-m-diameter PLF is a bisector (two-piece shell) fairing consisting of aluminum skin/stringer construction with vertical split-line longerons. The Atlas V 400 series oers three payload fairing options: the large (LPF, shown at left), the extended (EPF) and the extra extended (XPF). The 5-m PLF is a sandwich composite structure made with a vented aluminum-honeycomb core and graphite-epoxy face sheets. The bisector (two-piece shell) PLF encapsulates both the Centaur upper stage and the spacecraft, which separates using a debris-free pyrotechnic actuating 200 ft system. Payload clearance and vehicle structural stability are enhanced by the all-aluminum forward load reactor (FLR), which centers the PLF around the Centaur upper stage and shares payload shear loading. The Atlas V 500 series oers 1 three payload fairing options: the short (shown at left), medium 18 and long. 1 1 The Centaur upper stage is 3.1 m (10 ft) in diameter and 12.7 m (41.6 ft) long. Its propellant tanks are constructed of pressure-stabilized, corrosion-resistant stainless steel. Centaur is a liquid hydrogen/liquid oxygen-fueled vehicle. It uses a single RL10 engine producing 99.2 kN (22,300 lbf) of thrust. -
Evidence Review – Environmental Innovation Prizes for Development
Evidence Review – Environmental Innovation Prizes for Development DEW Point Enquiry No. A0405 A Report by Bryony Everett With support from Chris Barnett and Radha Verma Peer Review by William Masters July 2011 Acknowledgements We would like to thank all the interviewees detailed in Annex 1 for their time and support in providing us with their insights and information, without which we would not have been able to produce this report. Particular thanks go to Erika, Jaison and Will. Disclaimer This report is commissioned under DEW Point, the DFID Resource Centre for Environment, Water and Sanitation, which is managed by a consortium of companies led by Harewelle International Limited1. Although the report is commissioned by DFID, the views expressed in the report are entirely those of the authors and do not necessarily represent DFID’s own views or policies, or those of DEW Point. Comments and discussion on items related to content and opinion should be addressed to the author, via the “Contact and correspondence” address e-mail or website, as indicated in the control document above. 1 Consortium comprises Harewelle International Limited, DD International, Practical Action Consulting, Cranfield University and AEA Energy and Environment Table of Contents Evidence Review – Environmental Innovation Prizes for Development Summary .................................................................................................................................... 1 Introduction ............................................................................................................................. -
Phase Change: Titan’S Disappearing Lakes
Phase Change: Titan’s Disappearing Lakes Investigation Notebook NYC Edition © 2018 by The Regents of the University of California. All rights reserved. No part of this publication may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopy, recording, or any information storage or retrieval system, without permission in writing from the publisher. Teachers purchasing this Investigation Notebook as part of a kit may reproduce the book herein in sufficient quantities for classroom use only and not for resale. These materials are based upon work partially supported by the National Science Foundation under grant numbers DRL-1119584, DRL-1417939, ESI-0242733, ESI-0628272, and ESI-0822119. The Federal Government has certain rights in this material. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the author(s) and do not necessarily reflect the views of the National Science Foundation. These materials are based upon work partially supported by the Institute of Education Sciences, U.S. Department of Education, through Grant R305A130610 to The Regents of the University of California. The opinions expressed are those of the authors and do not represent views of the Institute or the U.S. Department of Education. Developed by the Learning Design Group at the University of California, Berkeley’s Lawrence Hall of Science. Amplify. 55 Washington Street, Suite 800 Brooklyn, NY 11201 1-800-823-1969 www.amplify.com Phase Change: Titan’s Disappearing Lakes -
Small Launch Vehicles a 2015 State of the Industry Survey Carlos Niederstrasser
Small Launch Vehicles A 2015 State of the Industry Survey Carlos Niederstrasser An update to this survey will be presented at the 2016 Internaonal Astronau9cal Congress 1 Agenda Overview of Small Launch Vehicles Launch Method/Locations Launch Performance Projected Launch Costs Individual Rocket Details Copyright © 2015 by Orbital ATK, Inc. 2 Listing Criteria Have a maximum capability to LEO of 1000 kg (definition of LEO left to the LV provider). The effort must be for the development of an entire launch vehicle system (with the exception of carrier aircraft for air launch vehicles). Mentioned through a web site update, social media, traditional media, conference paper, press release, etc. sometime after 2010. Have a stated goal of completing a fully operational space launch (orbital) vehicle. Funded concept or feasibility studies by government agencies, patents for new launch methods, etc., do not qualify. Expect to be widely available commercially or to the U.S. Government No specific indication that the effort has been cancelled, closed, or otherwise disbanded. Correc&ons, addi&ons, and comments are welcomed and encouraged! Copyright © 2015 by Orbital ATK, Inc. 3 We did not … … Talk to the individual companies … Rely on any proprietary/confidential information … Verify accuracy of data found in public resources Ø Primarily relied on companies’ web sites Funding sources, when listed, are not implied to be the vehicles sole or even majority funding source. We do not make any value judgements on technical or financial credibility -
A Low-Cost Launch Assistance System for Orbital Launch Vehicles
Hindawi Publishing Corporation International Journal of Aerospace Engineering Volume 2012, Article ID 830536, 10 pages doi:10.1155/2012/830536 Review Article A Low-Cost Launch Assistance System for Orbital Launch Vehicles Oleg Nizhnik ERATO Maenaka Human-Sensing Fusion Project, 8111, Shosha 2167, Hyogo-ken, Himeji-shi, Japan Correspondence should be addressed to Oleg Nizhnik, [email protected] Received 17 February 2012; Revised 6 April 2012; Accepted 16 April 2012 Academic Editor: Kenneth M. Sobel Copyright © 2012 Oleg Nizhnik. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. The author reviews the state of art of nonrocket launch assistance systems (LASs) for spaceflight focusing on air launch options. The author proposes an alternative technologically feasible LAS based on a combination of approaches: air launch, high-altitude balloon, and tethered LAS. Proposed LAS can be implemented with the existing off-the-shelf hardware delivering 7 kg to low-earth orbit for the 5200 USD per kg. Proposed design can deliver larger reduction in price and larger orbital payloads with the future advances in the aerostats, ropes, electrical motors, and terrestrial power networks. 1. Introduction point to the progress in the orbital delivery systems for these additional payload classes. Spaceflight is the mature engineering discipline—54 years old as of 2012. But seemingly paradoxically, it still relies solely 2. Overview of Previously Proposed LAS on the hardware and methodology developed in the very beginning of the spaceflight era. Modernly, still heavily-used A lot of proposals have been made to implement nonrocket Soyuz launch vehicle systems (LVSs) are the evolutionary LASandarelistedinTable 1. -
Spotlight on Asia-Pacific
Worldwide Satellite Magazine June 2008 SatMagazine Spotlight On Asia-Pacific * The Asia-Pacific Satellite Market Segment * Expert analysis: Tara Giunta, Chris Forrester, Futron, Euroconsult, NSR and more... * Satellite Imagery — The Second Look * Diving Into the Beijing Olympics * Executive Spotlight, Andrew Jordan * The Pros Speak — Mark Dankburg, Bob Potter, Adrian Ballintine... * Checking Out CommunicAsia + O&GC3 * Thuraya-3 In Focus SATMAGAZINE JUNE 2008 CONTENTS COVER FEATURE EXE C UTIVE SPOTLIGHT The Asia-Pacific Satellite Market Andrew Jordan by Hartley & Pattie Lesser President & CEO The opportunities, and challenges, SAT-GE facing the Asia-Pacific satellite market 12 are enormous 42 FEATURES INSIGHT Let The Games Begin... High Stakes Patent Litigation by Silvano Payne, Hartley & Pattie by Tara Giunta, Robert M. Masters, Lesser, and Kevin and Michael Fleck and Erin Sears The Beijing Olympic Games are ex- Like it or not, high stakes patent pected to find some 800,000 visitors wars are waging in the global satel- 47 arriving in town for the 17-day event. 04 lite sector, and it is safe to assume that they are here to stay. Transforming Satel- TBS: Looking At Further Diversification lite Broadband by Chris Forrester by Mark Dankberg Internationally, Turner Broadcasting The first time the “radical” concept has always walked hand-in-hand with 54 of a 100 Gbps satellite was intro- the growth of satellite and cable – duced was four years ago, 07 and now IPTV. Here’s Looking At Everything — Part II by Hartley & Pattie Lesser The Key To DTH Success In Asia by Jose del Rosario The Geostationary Operational Envi- Some are eyeing Asia as a haven for ronmental Satellites (GOES) continu- economic safety or even economic ously track evolution of weather over growth amidst the current global almost a hemisphere.