Sentinel-1A Launch
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Call for M5 Missions
ESA UNCLASSIFIED - For Official Use M5 Call - Technical Annex Prepared by SCI-F Reference ESA-SCI-F-ESTEC-TN-2016-002 Issue 1 Revision 0 Date of Issue 25/04/2016 Status Issued Document Type Distribution ESA UNCLASSIFIED - For Official Use Table of contents: 1 Introduction .......................................................................................................................... 3 1.1 Scope of document ................................................................................................................................................................ 3 1.2 Reference documents .......................................................................................................................................................... 3 1.3 List of acronyms ..................................................................................................................................................................... 3 2 General Guidelines ................................................................................................................ 6 3 Analysis of some potential mission profiles ........................................................................... 7 3.1 Introduction ............................................................................................................................................................................. 7 3.2 Current European launchers ........................................................................................................................................... -
AATSR Frequently Asked Questions (FAQ)
AATSR Frequently Asked Questions (FAQ) Author : IDEAS+ AATSR QC Team (Telespazio VEGA UK) IDEAS+-VEG-OQC-REP-2117 Issue 3 14 December 2016 AATSR Frequently Asked Questions (FAQ) Issue 3 AMENDMENT RECORD SHEET The Amendment Record Sheet below records the history and issue status of this document. ISSUE DATE REASON 1 20 Dec 2005 Initial Issue (as AEP_REP_001) 2 02 Oct 2013 Updated with new questions and information (issued as IDEAS- VEG-OQC-REP-0955) 3 14 Dec 2016 General updates, major edits to Q37., new questions: Q17., Q25., Q26., Q28., Q32., Q38., Q39., Q48. Now issued as IDEAS+-VEG-OQC-REP-2117 TABLE OF CONTENTS 1. INTRODUCTION ........................................................................................................................ 5 1.1 The Third AATSR Reprocessing Dataset (IPF 6.05) ............................................................ 5 1.2 References ............................................................................................................................ 6 2. GENERAL QUESTIONS ........................................................................................................... 7 Q1. What does AATSR stand for? ........................................................................................ 7 Q2. What is AATSR and what does it do? ............................................................................ 7 Q3. What is Envisat? ............................................................................................................. 7 Q4. What orbit does Envisat use? ........................................................................................ -
In Brief Modified to Increase Engine Reliability
r bulletin 102 — may 2000 3rd Space Station ESA, together with a European industrial Element to be Launched consortium headed by DaimlerChrysler (D) and including Belgian, Dutch and French NASA and the Russian Aviation and partners, was responsible for the design, Space Agency (Rosaviakosmos) plan that development and delivery of the core data the next component of the International management system, which provides Space Station (ISS) – the Zvezda service Zvezda’s main computer. module – will be launched on 12 July from the Baikonur Cosmodrome in Kazakhstan. ESA also has a contract with Rosaviakosmos and RSC-Energia for Following a Joint Programme Review and performing system and interface a General Designers’ Review in Moscow, it integration tasks required for docking with was agreed that Zvezda (Russian for Zvezda by ESA’s Automated Transfer ‘star’) will be launched by a Proton rocket Vehicle (ATV), which will be used for ISS with the second and third stage engines re-boost and logistics support missions In Brief modified to increase engine reliability. from 2003 onwards. Through its ATV industrial consortium led by Aerospatiale Zvezda will provide the early living quarters Matra Lanceurs (F), ESA is also procuring for ISS crew, together with the life sup- some Russian hardware and software for port, electrical power distribution, data use with the ATV. management, flight control, and propul- sion systems for the ISS. On the scientific side, ESA has concluded contracts with Rosaviakosmos and RSC- Energia for the conduct of scientific experiments on Zvezda, including the Global Timing System (GTS) and a radiobiology experiment (called Matroshka) to monitor and analyse radiation doses in ISS crew. -
Exploration of the Moon
Exploration of the Moon The physical exploration of the Moon began when Luna 2, a space probe launched by the Soviet Union, made an impact on the surface of the Moon on September 14, 1959. Prior to that the only available means of exploration had been observation from Earth. The invention of the optical telescope brought about the first leap in the quality of lunar observations. Galileo Galilei is generally credited as the first person to use a telescope for astronomical purposes; having made his own telescope in 1609, the mountains and craters on the lunar surface were among his first observations using it. NASA's Apollo program was the first, and to date only, mission to successfully land humans on the Moon, which it did six times. The first landing took place in 1969, when astronauts placed scientific instruments and returnedlunar samples to Earth. Apollo 12 Lunar Module Intrepid prepares to descend towards the surface of the Moon. NASA photo. Contents Early history Space race Recent exploration Plans Past and future lunar missions See also References External links Early history The ancient Greek philosopher Anaxagoras (d. 428 BC) reasoned that the Sun and Moon were both giant spherical rocks, and that the latter reflected the light of the former. His non-religious view of the heavens was one cause for his imprisonment and eventual exile.[1] In his little book On the Face in the Moon's Orb, Plutarch suggested that the Moon had deep recesses in which the light of the Sun did not reach and that the spots are nothing but the shadows of rivers or deep chasms. -
Echostar Annual Report Year Ended December 31, 2012 March 20, 2013
NASDAQ: SATS 100 Inverness Terrace East Englewood, CO 80112 303.706.4000 | echostar.com EchoStar Annual Report Year Ended December 31, 2012 March 20, 2013 Dear EchoStar Corporation Shareholders; 2012 was a very busy year for EchoStar. One of the most exciting accomplishments for 2012 was the addition of two new satellites to our growing fleet through the successful launches of EchoStar XVI and EchoStar XVII, bringing our total number of owned, leased and managed spacecraft to twenty-two. EchoStar operates the world’s fourth largest commercial geostationary satellite fleet and we continue to solidify our position as a premier global leader in satellite communications and operations. EchoStar ended 2012 with revenue of $3.1 billion, a growth of 13% over 2011. EBITDA in 2012 was $794 million, a growth of 64% over 2011. We generated a healthy $508 million of cash from operating activities in 2012 as a result primarily of the strong net income in 2012 and ended the year with a strong balance sheet with $1.5 billion of cash and marketable securities. EchoStar reached two very important long-term North America goals in 2012 with the market implementation of the HughesNet Gen4 service and the roll-out of the Hopper Whole Home DVR solution for DISH. Both solutions are garnering high praise and rapid adoption by consumers, a glowing testament to the capabilities and ingenuity of the EchoStar team. Additional notable accomplishments for 2012 include the very successful introduction of two new Slingbox retail products, several large enterprise contract renewals and new customers for Hughes data network services around the globe, and above-forecast sales of set-top-box products and video services to our established operator customers. -
Spacex CRS-4 National Aeronautics and Fourth Commercial Resupply Services Flight Space Administration
SpaceX CRS-4 National Aeronautics and Fourth Commercial Resupply Services Flight Space Administration to the International Space Station September 2014 OVERVIEW The Dragon spacecraft will be filled with more than 5,000 pounds of supplies and payloads, including critical materials to support 255 science and research investigations that will occur during Expeditions 41 and 42. Dragon will carry three powered cargo payloads in its pressurized section and two in its unpressurized trunk. Science payloads will enable model organism research using rodents, fruit flies and plants. A special science payload is the ISS-Rapid Scatterometer to monitor ocean surface wind speed and direction. Several new technology demonstrations aboard will enable bone density studies, test how a small satellite moves and positions itself in space using new thruster technology, and use the first 3-D printer in space for additive manufacturing. The mission also delivers IMAX cameras for filming during four increments and replacement batteries for the spacesuits. After four weeks at the space station, the spacecraft will return with about 3,800 pounds of cargo, including crew supplies, hardware and computer resources, science experiments, space station hardware, and four powered payloads. DRAGON CARGO LAUNCH ITEMS RETURN ITEMS TOTAL CARGO: 4885 lbs / 2216 kg 3276 lbs / 1486 kg · Crew Supplies 1380 lbs / 626 kg 132 lbs / 60 kg Crew care packages Crew provisions Food · Vehicle Hardware 403 lbs / 183 kg 937 lbs / 425 kg Crew Health Care System hardware Environment Control & Life Support equipment Electrical Power System hardware Extravehicular Robotics equipment Flight Crew Equipment Japan Aerospace Exploration Agency equipment · Science Investigations 1644 lbs / 746 kg 2075 lbs / 941 kg U.S. -
FAME-C: Cloud Property Retrieval Using Synergistic AATSR and MERIS Observations
Atmos. Meas. Tech., 7, 3873–3890, 2014 www.atmos-meas-tech.net/7/3873/2014/ doi:10.5194/amt-7-3873-2014 © Author(s) 2014. CC Attribution 3.0 License. FAME-C: cloud property retrieval using synergistic AATSR and MERIS observations C. K. Carbajal Henken, R. Lindstrot, R. Preusker, and J. Fischer Institute for Space Sciences, Freie Universität Berlin (FUB), Berlin, Germany Correspondence to: C. K. Carbajal Henken ([email protected]) Received: 29 April 2014 – Published in Atmos. Meas. Tech. Discuss.: 19 May 2014 Revised: 17 September 2014 – Accepted: 11 October 2014 – Published: 25 November 2014 Abstract. A newly developed daytime cloud property re- trievals. Biases are generally smallest for marine stratocu- trieval algorithm, FAME-C (Freie Universität Berlin AATSR mulus clouds: −0.28, 0.41 µm and −0.18 g m−2 for cloud MERIS Cloud), is presented. Synergistic observations from optical thickness, effective radius and cloud water path, re- the Advanced Along-Track Scanning Radiometer (AATSR) spectively. This is also true for the root-mean-square devia- and the Medium Resolution Imaging Spectrometer (MERIS), tion. Furthermore, both cloud top height products are com- both mounted on the polar-orbiting Environmental Satellite pared to cloud top heights derived from ground-based cloud (Envisat), are used for cloud screening. For cloudy pixels radars located at several Atmospheric Radiation Measure- two main steps are carried out in a sequential form. First, ment (ARM) sites. FAME-C mostly shows an underestima- a cloud optical and microphysical property retrieval is per- tion of cloud top heights when compared to radar observa- formed using an AATSR near-infrared and visible channel. -
NUCLEAR SAFETY LAUNCH APPROVAL: MULTI-MISSION LESSONS LEARNED Yale Chang the Johns Hopkins University Applied Physics Laboratory
ANS NETS 2018 – Nuclear and Emerging Technologies for Space Las Vegas, NV, February 26 – March 1, 2018, on CD-ROM, American Nuclear Society, LaGrange Park, IL (2018) NUCLEAR SAFETY LAUNCH APPROVAL: MULTI-MISSION LESSONS LEARNED Yale Chang The Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Rd, Laurel, MD 20723 240-228-5724; [email protected] Launching a NASA radioisotope power system (RPS) trajectory to Saturn used a Venus-Venus-Earth-Jupiter mission requires compliance with two Federal mandates: Gravity Assist (VVEJGA) maneuver, where the Earth the National Environmental Policy Act of 1969 (NEPA) Gravity Assist (EGA) flyby was the primary nuclear safety and launch approval (LA), as directed by Presidential focus of NASA, the U.S. Department of Energy (DOE), the Directive/National Security Council Memorandum 25. Cassini Interagency Nuclear Safety Review Panel Nuclear safety launch approval lessons learned from (INSRP), and the public alike. A solid propellant fire test multiple NASA RPS missions, one Russian RPS mission, campaign addressed the MPF finding and led in part to two non-RPS launch accidents, and several solid the retrofit solid propellant breakup systems (BUSs) propellant fire test campaigns since 1996 are shown to designed and carried by MER-A and MER-B spacecraft have contributed to an ever-growing body of knowledge. and the deployment of plutonium detectors in the launch The launch accidents can be viewed as “unplanned area for PNH. The PNH mission decreased the calendar experiments” that provided real-world data. Lessons length of the NEPA/LA processes to less than 4 years by learned from the nuclear safety launch approval effort of incorporating lessons learned from previous missions and each mission or launch accident, and how they were tests in its spacecraft and mission designs and their applied to improve the NEPA/LA processes and nuclear NEPA/LA processes. -
PRESS-KIT-VV19-08122021-EN.Pdf
www.arianespace.com www.avio.com www.avio Arianespace’s seventh launch of 2021 with the second Vega of the year will place its satellite passengers into Sun-synchronous orbit. The launcher will be carrying a total payload of approximately 1 029 kg. The launch will be performed in Kourou, French Guiana. MISSION DESCRIPTION 2 PLÉIADES NEO 4 SATELLITE 3 Liftoff is planned on at exactly: FOUR AUXILIARY PAYLOADS 4 - 5 09:47 p.m. Washington, D.C. time, 10:47 p.m. Kourou time, VEGA LAUNCHER 6 01:47 a.m. Universal time (UTC), August 17, LAUNCH CAMPAIGN 7 03:47 a.m. Paris time, August 17, 10:47 a.m. Tokyo time, August 17. FLIGHT SEQUENCES 7 STAKEHOLDERS OF A LAUNCH 8 The nominal duration of the mission (from liftoff to separation of the satellites) is: 1 hour, 44 minutes and 59 seconds. Satellite: Pléiades Neo 4 Customer: Airbus Defence and Space - Intelligence Satellites: Four auxiliary payloads Cyrielle BOUJU [email protected] +33 (0)6 32 65 97 48 For Pléiades Neo For the four auxiliary payloads Francesco DE LORENZO • Perigee altitude: 614 km • Perigee altitude: 540 km [email protected] • Apogee altitude: 625 km • Apogee altitude: 554 km + 39 (0)6 97285317 • Inclination : 97.89 degrees • Inclination : 97.55 degrees First Pléiades Neo constellation satellites have been achieved within only five years, thanks to the hard work of over 500 people, across seven sites in Europe, to deliver first-class 14 km swath imagery at 30 cm native resolution, capable to daily collect up to 2 million km² and image the entire Earth landmass five times per year. -
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. -
Final Report Cover Ar
Authors ASIS Melanie Clegg U.S.A. Julie Mason U.S.A. Vincent Coache Canada Narasimha Murthy N. Narasimhulu India Tyler Dwyer Canada Paul Nizenkov Germany Shady El Azab Belgium Duarte Sousa Portugal Kristin Freeman U.S.A. Fredrik Persson Sweden Shai Gerner Israel Udrivolf Pica Italy Marc Gick Canada Lucie Poulet France Fei Guan China Maxime Puteaux France Yuri Ishizu Japan Dmitry Rachkin Russian Federation Operations Sebastian Klaus Germany Eirini Maria Sfantzikaki Greece Marc Labriet U.S.A. Yuan Si China And Service Mikkel Ladegaard Denmark Chrishma Singh-Derewa U.S.A. Frederico Larangeira Portugal Rui Sousa Portugal Luliang Lou China Suki Dauda Sule Nigeria Infrastructure Zhuoyan Lu China Anna Szwemin Poland Qinglang Luo China Graeme Taylor United Kingdom for Space Nuno Loureiro Portugal Aliya Valiyff Australia Final Report SPACE STUDIES PROGRAM 2012 INTERNATIONAL SPACE UNIVERSITY | FLORIDA INSTITUTE OF TECHNOLOGY | KENNEDY SPACE CENTER Operations and Service Infrastructure for Space Team Project: Spaceports Team Project Report International Space University SSP 2012 © International Space University. All Rights Reserved. The SSP 2012 Program of the International Space University was held at Florida Institute of Technology, Melbourne, Florida, USA. The OASIS concept is represented in the cover artwork and logo. Within the logo are the nodes representing the spaceport way-points. It was inspired by the skipping of stones across a body of water, representing stepping stones throughout space. The abstract palm tree represents the OASIS concept - a location where you gather supplies and services while traveling through a harsh environment. Design work courtesy of the OASIS Graphics Team. While all care has been taken in the preparation of this report, the International Space University (ISU) does not take any responsibility for the accuracy of its content. -
Sentinel-3 Product Notice
Copernicus S3 Product Notice – Altimetry Mission S3 Sensor SRAL / MWR Product LAND L2 NRT, STC and NTC Product Notice ID S3A.PN-STM-L2L.10 Issue/Rev Date 16/07/2020 Version 1.1 This Product Notice was prepared by the S3 Mission Performance Centre Preparation and ESA experts Approval ESA Mission Management Summary This is a Product Notice (PN) for the Copernicus Sentinel-3A and Sentinel-3B Surface Topography Mission (STM) Level-2 Land products at Near Real Time (NRT), Short Time Critical (STC) and Non Time Critical (NTC) timeliness. The Notice describes the STM current status, product quality and limitations, and product availability status. © ESA page 1 / 16 Processing Baseline S3A S3B Processing Baseline • Processing Baseline: 2.68 • Processing Baseline: 1.42 • • SR_1 IPF version: 06.18 SR_1 IPF version: 06.18 • MW_1 IPF version: 06.11 IPFs version • MW_1 IPF version: 06.11 • • SM_2 IPF version: 06.19 SM_2 IPF version: 06.19 Current Operational Processing Baseline IPF IPF Version In OPE since S3A SR1 06.18 Land Centres: NRT mode : 2020-07-09 STC mode : 2020-07-09 NTC mode : 2020-07-09 S3A MW1 06.11 Land Centres: NRT mode : 2020-01-21 STC mode : 2020-01-21 NTC mode : 2020-01-21 S3A SM2 06.19 Land Centres: NRT mode : 2020-07-09 STC mode : 2020-07-09 NTC mode : 2020-07-09 S3B SR1 06.18 Land Centres: NRT mode : 2020-07-09 STC mode : 2020-07-09 NTC mode : 2020-07-09 S3B MW1 06.11 Land Centres: NRT mode : 2020-01-21 STC mode : 2020-01-21 NTC mode : 2020-01-21 S3B SM2 06.19 Land Centres: NRT mode : 2020-07-09 STC mode : 2020-07-09 NTC mode : 2020-07-09 © ESA page 2 / 16 Status of the Processing Baseline S3A The Processing Baseline (PB) for Copernicus Sentinel-3A STM products associated to this PN is reported above.