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Attachment J-4 Applicable and Reference Documents Lists
NNJ12GA46C SECTION J Attachment J-4 MISSION AND PROGRAM INTEGRATION CONTRACT Attachment J-4 Applicable and Reference Documents Lists J-A4-1 NNJ12GA46C SECTION J Attachment J-4 MISSION AND PROGRAM INTEGRATION CONTRACT This attachment contains applicable documents for the contract effort. The contractor shall comply with these requirements in performing Statement of Work (SOW) requirements. This attachment is structured as follows: Table J4-1: Applicable Documents List Table J4-2: Reference Documents List Table J4-3: Book Editor/Book Coordinated/Managed Documents List Table J4-4: Orion Documents List The documents identified within Table J4-1 or within a document listed in this table (second tier) are applicable to this contract. Requirements written in these documents have full force and effect as if their text were written in this contract to the extent that the requirements relate to context of the work to be performed within the scope of this contract. When a document is classified as “reference,” the document is provided for information about the ISS Program execution and the Mission and Program Integration Contract’s role in the ISS Program. The general approach for interpreting whether a document impacts the contractor’s performance is that if a document is “applicable,” then the contractor has solid requirements that derive from that document. Applicable documents contain additional requirements and are considered binding to the extent specified. Applicable documents cited in the text of the document in a manner that indicates applicability such as follows: • In accordance with • As stated in • As specified in • As defined in • Per • In conformance with When a document is classified as “reference,” the document is provided for general context of the ISS Program execution and for influence on the performance of the Mission and Program Integration Contract in its role of support to the ISS Program. -
How a Cartoon Series Helped the Public Care About Rosetta and Philae 13 How a Cartoon Series Helped the Public Care About Rosetta and Philae
How a Cartoon Series Helped the Public Care about Best Practice Rosetta and Philae Claudia Mignone Anne-Mareike Homfeld Sebastian Marcu Vitrociset Belgium for European Space ATG Europe for European Space Design & Data GmbH Agency (ESA) Agency (ESA) [email protected] [email protected] [email protected] Carlo Palazzari Emily Baldwin Markus Bauer Design & Data GmbH EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) [email protected] [email protected] [email protected] Keywords Karen S. O’Flaherty Mark McCaughrean Outreach, space science, public engagement, EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) visual storytelling, fairy-tale, cartoon, animation, [email protected] [email protected] anthropomorphising Once upon a time... is a series of short cartoons1 that have been developed as part of the European Space Agency’s communication campaign to raise awareness about the Rosetta mission. The series features two anthropomorphic characters depicting the Rosetta orbiter and Philae lander, introducing the mission story, goals and milestones with a fairy- tale flair. This article explores the development of the cartoon series and the level of engagement it generated, as well as presenting various issues that were encountered using this approach. We also examine how different audiences responded to our decision to anthropomorphise the spacecraft. Introduction internet before the spacecraft came out of exciting highlights to come, using the fairy- hibernation (Bauer et al., 2016). The four tale narrative as a base. The hope was that In late 2013, the European Space Agency’s short videos were commissioned from the video would help to build a degree of (ESA) team of science communicators the cross-media company Design & Data human empathy between the public and devised a number of outreach activ- GmbH (D&D). -
Jules Verne ATV Launch Approaching 11 February 2008
Jules Verne ATV launch approaching 11 February 2008 will carry up to 9 tonnes of cargo to the station as it orbits 400 km above the Earth. Equipped with its own propulsion and navigation systems, the ATV is a multi-functional spacecraft, combining the fully automatic capabilities of an unmanned vehicle with the safety requirements of a crewed vehicle . Its mission in space will resemble that, on the ground, of a truck (the ATV) delivering goods and services to a research establishment (the space station). A new-generation high-precision navigation system will guide the ATV on a rendezvous trajectory towards the station. In early April, Jules Verne will automatically dock with the station’s Russian Preview of the maiden launch and docking of ESA's Jules Verne ATV. Jules Verne will be lifted into space on Service Module, following a number of specific board an Ariane 5 launch vehicle. Credits: ESA - D. operations and manoeuvres (on 'Demonstration Ducros Days') to show that the vehicle is performing as planned in nominal and contingency situations. It will remain there as a pressurised and integral After the successful launch of ESA’s Columbus part of the station for up to six months until a laboratory aboard Space Shuttle Atlantis on controlled re-entry into the Earth’s atmosphere Thursday (7 February), it is now time to focus on takes place, during which it will burn up and, in the the next imminent milestone for ESA: the launch of process, dispose of 6.3 tonnes of waste material no Jules Verne, the first Automated Transfer Vehicle longer needed on the station. -
Level Ministerial and Scientific Event a New Era of Blue Enlightenment
Report on the High- Level Ministerial and Scientific Event A New Era of Blue Enlightenment 12-14 July 2017 Lisbon, Portugal October 2017 EUROPEAN COMMISSION Directorate-General for Research and Innovation Directorate F — Bioeconomy Unit F.4 — Marine Resources Contact: Sieglinde Gruber E-mail: [email protected] [email protected] European Commission B-1049 Brussels EUROPEAN COMMISSION Report on the High-Level Ministerial and Scientific Event A New Era of Blue Enlightenment 12-14 July 2017 Directorate-General for Research and Innovation 2017 Bioeconomy EN 3 EUROPE DIRECT is a service to help you find answers to your questions about the European Union Freephone number (*): 00 800 6 7 8 9 10 11 (*) The information given is free, as are most calls (though some operators, phone boxes or hotels may charge you) LEGAL NOTICE This document has been prepared for the European Commission however it reflects the views only of the authors, and the Commission cannot be held responsible for any use which may be made of the information contained therein. More information on the European Union is available on the internet (http://europa.eu). Luxembourg: Publications Office of the European Union, 2016. PDF ISBN 978-92-79-73529-5 doi: 10.2777/64644 KI-04-17-849-EN-N © European Union, 2017. Reproduction is authorised provided the source is acknowledged. Cover images: © Lonely, # 46246900, 2011. © ag visuell #16440826, 2011. © Sean Gladwell #6018533, 2011. © LwRedStorm, #3348265. 2011. © kras99, #43746830, 2012. Source: Fotolia.com Internal document image(s): © European Union, 2017, Source: EC - Audiovisual Service, Photo: Bruno Portela 3 "The Sea, the great unifier, is man's only hope. -
Balloon Powered Phoenix Mars Lander Model (Simplified Version)
balloon powered Phoenix Mars Lander Model (simplified version) by Steve Widmark Mountain View High School, Mountain View, CA What is Phoenix? Phoenix is NASA’s latest mission to Mars. Launched on a Delta II rocket on August 4 th , 2007, the Phoenix lander will touch down in the northern region of Mars on May 25, 2008. Once there, it will dig into the Martian permafrost using a robotic arm and analyze the composition of the soil and ice it removes with a sophisticated automated laboratory. In a nutshell, the goal of the mission is to determine if the Martian surface is (or was) capable of supporting life. Unlike the previous rover missions to Mars that made bounce landings using air bags, Phoenix will make a powered landing employing twelve thrusters positioned around the spacecraft. The model demonstrates this method of landing with a single balloon “thruster.” For more information about the Phoenix mission go to http://phoenix.lpl.arizona.edu Materials and tools: 1 parts sheet color printed on 110 lb (#110) card stock 1 balloon (lander flies best with a 5” balloon) 1 small paper clip clear tape glue sick or white glue scissors pencil Directions: Note: If the directions tell you to bend a tab down, this means to bend the tab down with the printed portion of the part facing up. If the directions tell you to bend a tab up, this means to bend the tab up with the printed portion of the part facing up. The front side of a part is the side with the printing. -
EUMETSAT Water Vapour Products from New Generation Satellites
EUMETSAT water vapour imagery products from new generation satellites: development and validation strategy L. Spezzi*, P. Watts, B. Fougnie, J. Chimot, E. Obligis, B. Bojkov *[email protected] 1 EUMETSAT Water Vapor Imagery products @ G-VAP Meeting (Madrid, 13/14 June 2019) Water Vapour Product map (missions & products) EUMETSAT instrumentation: IR and MW sounders, MW imagers, VIS/IR imagers, UV/VIS spectrometers Operational In development Possible Planned only Not yet committed/under study Not Applicable (not yet in plan → room for @EUMETSAT @SAFs @EUMETSAT @EUMETSAT improvement) and/or SAFs and/or SAFs E.g. talk by Sküchler: “Total water vapor column from Sentinel-5P derived by the AMC-DOAS method” Instr./ Metop MSG Sentinel 3 Metop-SG MTG AMSU IASI S5 S4 AVHRR IASI MWR MWI ICI MWS IRS Product MHS SEVIRI OLCI SLSTR VII 3MI NG UVNS FCI UVN Total Colum Water Vapour (clear-sky) Layer Precipitable Water 1=surface to 850hPa 2=850 to 500 hPa 3=500 hPa to TOA Humidity profile 2004 to present 2016 2022+ Time to present Talk by T. August: ‘’IASI retrieval and validation activities at EUMETSAT: Recent updates’’ 2 EUMETSAT Water Vapor Imagery products @ G-VAP Meeting (Madrid, 13/14 June 2019) EUMETSAT sensors for water vapour imagery High spatial resolution Main types of sensors providing imaging measurements for water vapour retrieval Current: • Multispectral Pushbroom and Dual-view radiometer: →Sentinel-3/OLCI and SLSTR ECMWF does not always S3/OLCI (300m) • Geostationary multi-spectral imagers: resolve all features →MSG/SEVIRI Future: • Geostationary multi-spectral imagers: →MTG/FCI • Polar multi-spectral imagers: →EPS-SG/METimage • Multi-directional Polarimeter: • WV concentration in the boundary layer is an indicator of →EPS-SG/3MI mesoscale developments (scale ~4km), e.g. -
Space Sector Brochure
SPACE SPACE REVOLUTIONIZING THE WAY TO SPACE SPACECRAFT TECHNOLOGIES PROPULSION Moog provides components and subsystems for cold gas, chemical, and electric Moog is a proven leader in components, subsystems, and systems propulsion and designs, develops, and manufactures complete chemical propulsion for spacecraft of all sizes, from smallsats to GEO spacecraft. systems, including tanks, to accelerate the spacecraft for orbit-insertion, station Moog has been successfully providing spacecraft controls, in- keeping, or attitude control. Moog makes thrusters from <1N to 500N to support the space propulsion, and major subsystems for science, military, propulsion requirements for small to large spacecraft. and commercial operations for more than 60 years. AVIONICS Moog is a proven provider of high performance and reliable space-rated avionics hardware and software for command and data handling, power distribution, payload processing, memory, GPS receivers, motor controllers, and onboard computing. POWER SYSTEMS Moog leverages its proven spacecraft avionics and high-power control systems to supply hardware for telemetry, as well as solar array and battery power management and switching. Applications include bus line power to valves, motors, torque rods, and other end effectors. Moog has developed products for Power Management and Distribution (PMAD) Systems, such as high power DC converters, switching, and power stabilization. MECHANISMS Moog has produced spacecraft motion control products for more than 50 years, dating back to the historic Apollo and Pioneer programs. Today, we offer rotary, linear, and specialized mechanisms for spacecraft motion control needs. Moog is a world-class manufacturer of solar array drives, propulsion positioning gimbals, electric propulsion gimbals, antenna positioner mechanisms, docking and release mechanisms, and specialty payload positioners. -
Institut Für Weltraumforschung (IWF) Österreichische Akademie Der Wissenschaften (ÖAW) Schmiedlstraße 6, 8042 Graz, Austria
WWW.OEAW.AC.AT ANNUAL REPORT 2018 IWF INSTITUT FÜR WELTRAUMFORSCHUNG WWW.IWF.OEAW.AC.AT ANNUAL REPORT 2018 COVER IMAGE Artist's impression of the BepiColombo spacecraft in cruise configuration, with Mercury in the background (© spacecraft: ESA/ATG medialab; Mercury: NASA/JPL). TABLE OF CONTENTS INTRODUCTION 5 NEAR-EARTH SPACE 7 SOLAR SYSTEM 13 SUN & SOLAR WIND 13 MERCURY 15 VENUS 16 MARS 17 JUPITER 18 COMETS & DUST 20 EXOPLANETARY SYSTEMS 21 SATELLITE LASER RANGING 27 INFRASTRUCTURE 29 OUTREACH 31 PUBLICATIONS 35 PERSONNEL 45 IMPRESSUM INTRODUCTION INTRODUCTION The Space Research Institute (Institut für Weltraum- ESA's Cluster mission, launched in 2000, still provides forschung, IWF) in Graz focuses on the physics of space unique data to better understand space plasmas. plasmas and (exo-)planets. With about 100 staff members MMS, launched in 2015, uses four identically equipped from 20 nations it is one of the largest institutes of the spacecraft to explore the acceleration processes that Austrian Academy of Sciences (Österreichische Akademie govern the dynamics of the Earth's magnetosphere. der Wissenschaften, ÖAW, Fig. 1). The China Seismo-Electromagnetic Satellite (CSES) was IWF develops and builds space-qualified instruments and launched in February to study the Earth's ionosphere. analyzes and interprets the data returned by them. Its core engineering expertise is in building magnetometers and NASA's InSight (INterior exploration using Seismic on-board computers, as well as in satellite laser ranging, Investigations, Geodesy and Heat Transport) mission was which is performed at a station operated by IWF at the launched in May to place a geophysical lander on Mars Lustbühel Observatory. -
The Extreme Physical Properties of the Corot-7B Super-Earth
1 08/02/2011 The extreme physical properties of the CoRoT-7b super-Earth A. Légera,b, O. Grassetc, B. Fegleyd, F. Codrone, A., F. Albaredef, P. Bargeg, R. Barnesh, P. Cancec, S. Carpyc, F. Catalanoi, C. Cavarroca,b, O. Demangeona,b, S. Ferraz-Melloj, P. Gabora,b, J.-M. Grießmeierk, J. Leibachera,b,q, G. Libourell, A-S. Maurinl,q , S.N. Raymondl,q , D. Rouann, B. Samuela, L. Schaeferc, J. Schneidero, P. A. Schullera, F. Selsisl,q , C. Sotinp. Affiliations a. (Corresponding author) Institut d’Astrophysique Spatiale, Université Paris-Sud, bât 121, Univ. Paris-Sud, F-91405 Orsay, France; e-mail: [email protected]; ph: 33 1 69 85 85 80 b. Institut d’Astrophysique Spatiale, CNRS (UMR 8617), bât 121, Univ. Paris-Sud, F- 91405 Orsay, France, c. Université de Nantes, CNRS, Lab de planétologie et Géodynamique, UMR- CNRS 6112, F-44300 Nantes d. Planetary Chemistry Laboratory McDonnell Center for the Space Sciences, Dep. of Earth and Planetary Sciences, Washington University in St. Louis, USA; e. Laboratoire de Météorologie Dynamique CNRS/UPMC, T 45-55, E3, 75252 Paris Cedex 05 – France; f. Ecole Normale Supérieure (LST), 69364 Lyon cedex 7, France; Laboratoire d’Astrophysique de Marseille, Pôle de l'Étoile, 38 r. Frédéric Joliot-Curie, 13388 Marseille cedex 13, France g. Department of Astronomy, University of Washington, Seattle, WA, 98195-1580, USA; h. 12 av. Fontaine de la Reine, 92430 Marnes la Coquette, France; i. IAG-Universidade de Sao Paulo, Brasil; j. Centre de Biophysique Moléculaire CNRS, r. Charles Sadron, 45071 Orléans cedex 2, France; k. -
First Year of Coordinated Science Observations by Mars Express and Exomars 2016 Trace Gas Orbiter
MANUSCRIPT PRE-PRINT Icarus Special Issue “From Mars Express to ExoMars” https://doi.org/10.1016/j.icarus.2020.113707 First year of coordinated science observations by Mars Express and ExoMars 2016 Trace Gas Orbiter A. Cardesín-Moinelo1, B. Geiger1, G. Lacombe2, B. Ristic3, M. Costa1, D. Titov4, H. Svedhem4, J. Marín-Yaseli1, D. Merritt1, P. Martin1, M.A. López-Valverde5, P. Wolkenberg6, B. Gondet7 and Mars Express and ExoMars 2016 Science Ground Segment teams 1 European Space Astronomy Centre, Madrid, Spain 2 Laboratoire Atmosphères, Milieux, Observations Spatiales, Guyancourt, France 3 Royal Belgian Institute for Space Aeronomy, Brussels, Belgium 4 European Space Research and Technology Centre, Noordwijk, The Netherlands 5 Instituto de Astrofísica de Andalucía, Granada, Spain 6 Istituto Nazionale Astrofisica, Roma, Italy 7 Institut d'Astrophysique Spatiale, Orsay, Paris, France Abstract Two spacecraft launched and operated by the European Space Agency are currently performing observations in Mars orbit. For more than 15 years Mars Express has been conducting global surveys of the surface, the atmosphere and the plasma environment of the Red Planet. The Trace Gas Orbiter, the first element of the ExoMars programme, began its science phase in 2018 focusing on investigations of the atmospheric composition with unprecedented sensitivity as well as surface and subsurface studies. The coordination of observation programmes of both spacecraft aims at cross calibration of the instruments and exploitation of new opportunities provided by the presence of two spacecraft whose science operations are performed by two closely collaborating teams at the European Space Astronomy Centre (ESAC). In this paper we describe the first combined observations executed by the Mars Express and Trace Gas Orbiter missions since the start of the TGO operational phase in April 2018 until June 2019. -
Insight Spacecraft Launch for Mission to Interior of Mars
InSight Spacecraft Launch for Mission to Interior of Mars InSight is a robotic scientific explorer to investigate the deep interior of Mars set to launch May 5, 2018. It is scheduled to land on Mars November 26, 2018. It will allow us to better understand the origin of Mars. First Launch of Project Orion Project Orion took its first unmanned mission Exploration flight Test-1 (EFT-1) on December 5, 2014. It made two orbits in four hours before splashing down in the Pacific. The flight tested many subsystems, including its heat shield, electronics and parachutes. Orion will play an important role in NASA's journey to Mars. Orion will eventually carry astronauts to an asteroid and to Mars on the Space Launch System. Mars Rover Curiosity Lands After a nine month trip, Curiosity landed on August 6, 2012. The rover carries the biggest, most advanced suite of instruments for scientific studies ever sent to the martian surface. Curiosity analyzes samples scooped from the soil and drilled from rocks to record of the planet's climate and geology. Mars Reconnaissance Orbiter Begins Mission at Mars NASA's Mars Reconnaissance Orbiter launched from Cape Canaveral August 12. 2005, to find evidence that water persisted on the surface of Mars. The instruments zoom in for photography of the Martian surface, analyze minerals, look for subsurface water, trace how much dust and water are distributed in the atmosphere, and monitor daily global weather. Spirit and Opportunity Land on Mars January 2004, NASA landed two Mars Exploration Rovers, Spirit and Opportunity, on opposite sides of Mars. -
A Launch for the International Space Station
A launch for the International Space Station For its first mission of the year, Arianespace will launch the first Automated Transfer Vehicle (ATV), dubbed “Jules Verne”, for the European Space Agency (ESA). Right from this first launch, the ATV will play a vital role in bringing supplies to the International Space Station (ISS). Weighing more than 20 tons, this will be by far the heaviest payload ever launched by Ariane 5. An Ariane 5 ES will inject the Jules Verne ATV into a circular orbit at an altitude of 260 kilometers, inclined 51.6 degre e s . With this launch, Ariane 5 further expands its array of missions, ranging fro m scientific spacecraft in special orbits to commercial launches into geostationary orbit. The ATV is designed to bring supplies to the ISS (water, air, food, propellants for the Russian section, spare parts, experimental hard w a re, etc.), and to reboost the ISS into its nominal orbit. The ISS now weighs more than 240 metric tons, including the recently attached European labora t o r y, Columbus. After being docked to the ISS for up to six months, the ATV will be loaded with waste items by the astronauts, and sent back down. After separating from the launch vehicle, the ATV will be autonomous, using its own systems for energy (batteries and four large solar panels) and guidance (GPS, star t racker), in liaison with the control center in Toulouse. During final approach, an optical navigation system will guide the ATV to its rendezvous with the Space Station, w h e re it will automatically dock several days after launch.