CDF Study Report: CDF-145(C) June 2014 Page 1 of 254

Total Page:16

File Type:pdf, Size:1020Kb

CDF Study Report: CDF-145(C) June 2014 Page 1 of 254 Phobos SR CDF Study Report: CDF-145(C) June 2014 page 1 of 254 CDF Study Report Phobos Sample Return Phobos Moon of Mars Sample Return Mission ESA UNCLASSIFIED – Releasable to the Public Phobos SR CDF Study Report: CDF-145(C) June 2014 page 2 of 254 This study is based on the ESA CDF Integrated Design Model (IDM), which is copyright 2004 – 2012 by ESA. All rights reserved. Further information and/or additional copies of the report can be requested from: D. Rebuffat ESA/ESTEC/SRE-FMP Postbus 299 2200 AG Noordwijk The Netherlands Tel: +31-(0)71-5655174 Fax: +31-(0)71-5655985 [email protected] For further information on the Concurrent Design Facility please contact: M. Bandecchi ESA/ESTEC/TEC-SYE Postbus 299 2200 AG Noordwijk The Netherlands Tel: +31-(0)71-5653701 Fax: +31-(0)71-5656024 [email protected] FRONT COVER Study logo showing Phobos Sample Return Stack with Mars and Phobos and Deimos in the background ESA UNCLASSIFIED – Releasable to the Public Phobos SR CDF Study Report: CDF-145(C) June 2014 page 3 of 254 STUDY TEAM This study was performed in the ESTEC Concurrent Design Facility (CDF) by the following interdisciplinary team: TEAM LEADER AEROTHERMO PAYLOAD/ DYNAMICS DETECTORS GNC POWER COMMUNICATIONS PROGRAMMATICS/ AIV CONFIGURATION PROPULSION COST RISK DATA HANDLING ROBOTICS GS&OPS STRUCTURES MECHANISMS SYSTEMS MISSION ANALYSIS THERMAL Under the responsibility of: SRE-FMP, Study Manager SRE-FMP, Study Responsible With the technical support of SRE-FMP, System Support TEC-MSM, Mechanisms (simulations) SRE-FMP, Observer SRE-FMP, Observer With the scientific assistance of: IKI, Study Scientist SRE-S, Study Scientist With the involvement of: IKI, Technical Support on Sampling chain IKI, Technical Support on Sampling chain IKI, Technical Support on Sampling chain ESA UNCLASSIFIED – Releasable to the Public Phobos SR CDF Study Report: CDF-145(C) June 2014 page 4 of 254 Lavochkin, Technical Support on ERV and PM Lavochkin, Technical Support on ERV and PM Lavochkin, Technical Support on ERV and PM The editing and compilation of this report has been provided by: A. Pickering, TEC-SYE, Technical Author ESA UNCLASSIFIED – Releasable to the Public Phobos SR CDF Study Report: CDF-145(C) June 2014 page 5 of 254 TABLE OF CONTENTS 1 INTRODUCTION .................................................................................. 13 1.1 Background .............................................................................................................13 1.2 Scope .......................................................................................................................13 1.3 Document Structure ................................................................................................13 2 EXECUTIVE SUMMARY ...................................................................... 15 2.1 Study Flow ............................................................................................................... 15 2.2 Mission Objectives and Requirements ................................................................... 15 2.3 Phobos Sample Return Mission Architecture ....................................................... 16 2.4 Phobos Sample Return Composite ........................................................................ 18 2.5 Phobos Sample Return Elements .......................................................................... 19 2.5.1 Earth Re-entry Capsule ................................................................................... 19 2.5.2 Earth Return Vehicle ....................................................................................... 20 2.5.3 Landing Module ............................................................................................... 20 2.5.4 Propulsion Module .......................................................................................... 21 2.6 Conclusions and Options ....................................................................................... 22 3 MISSION OBJECTIVES ....................................................................... 23 3.1 Background ............................................................................................................ 23 3.2 Science Objectives .................................................................................................. 23 3.3 Technology Objectives ........................................................................................... 23 3.4 Options ................................................................................................................... 24 3.5 Study Objectives ..................................................................................................... 25 3.6 Mission and System Requirements ....................................................................... 25 4 MISSION ANALYSIS ............................................................................ 27 4.1 Requirements and Design Drivers ......................................................................... 27 4.2 Assumptions and Trade-Offs ................................................................................. 27 4.3 Baseline Design ...................................................................................................... 27 4.3.1 Launch and Earth Escape Sequence................................................................ 27 4.3.2 Outbound Transfers ......................................................................................... 28 4.4 Budgets ................................................................................................................... 28 4.4.1 Short Transfers ................................................................................................ 29 4.4.2 Long Transfers ................................................................................................. 29 4.4.3 Earth Swing-by Transfers ................................................................................ 30 4.4.4 Near Phobos Operations .................................................................................. 30 4.4.5 Earth Return .................................................................................................... 30 4.5 Options ................................................................................................................... 30 4.5.1 Transfer from Deimos to Phobos Orbit ........................................................... 30 5 PAYLOAD ............................................................................................ 31 5.1 Requirements and Design Drivers ..........................................................................31 ESA UNCLASSIFIED – Releasable to the Public Phobos SR CDF Study Report: CDF-145(C) June 2014 page 6 of 254 5.2 Assumptions and Trade-Offs ................................................................................. 31 5.3 Baseline Design and Characteristic of Model Payload Instruments; Category I (Instruments Mounted on LM Only) ............................................................................ 31 5.3.1 Wide Angle Camera - WAC .............................................................................. 32 5.3.2 Narrow Angle Camera – NAC and CSU .......................................................... 32 5.3.3 Stereo Camera – StereoCam ............................................................................ 32 5.3.4 Close-Up Imager – CLUPI ............................................................................... 32 5.3.5 Visible Near Infrared Spectrometer – VisNIR ................................................ 33 5.3.6 Mid Infrared Spectrometer – MidIR ............................................................... 33 5.3.7 Neutron Spectrometer - ADRON-RM ............................................................. 33 5.3.8 Dust Detector - DIAMOND ............................................................................. 33 5.3.9 Starfield Observation – LIBRATION .............................................................. 34 5.3.10 Radio Science Experiment ............................................................................... 34 5.4 Optional Instruments; Category II (Instruments Mounted on LM Only) ............ 34 5.5 Optional Instruments Category III (Instruments Mounted on ERV and/or ERC)35 5.5.1 BIOPhobos Experiment ................................................................................... 35 5.5.2 TV Camera ........................................................................................................ 35 5.6 List of Equipment ................................................................................................... 35 5.7 Technology Requirements ..................................................................................... 38 6 PROPULSION MODULE (BASELINE) .................................................. 39 6.1 Study Assumptions ................................................................................................. 39 6.2 Design Description ................................................................................................. 39 6.3 Options ................................................................................................................... 41 6.4 Interface Requirements.......................................................................................... 42 6.5 Technology Requirements ..................................................................................... 43 7 EARTH RETURN VEHICLE .................................................................
Recommended publications
  • Benchmark Literacy Overview Common Core Edition
    BENCHMARK BENCHMARK LITERACYTM LITERACYTM GRADE TM Why choose Benchmark Literacy over K–6 all the other K–6 reading programs? Overview Common Core Edition Common Core Edition • Ten comprehension-focused units per grade • Grade-specific leveled text collections with explicit model-guide-apply instruction organized by unit comprehension strategy Needs • Seamless, spiraling, whole- to small-group • Phonics and word study kits that provide instruction that supports curriculum standards a complete K –6 continuum of skills • Pre-, post-, and ongoing assessment that • Research-proven instructional design Vocabulary drives instruction Shared Reading Phonics & Word Study Fluency Word Study Phonics Independent Reading Comprehensionp K–6 Comprehensive Teacher Resource Systems Assessment & Instruction $95.00 Y13229 B e n c h m a r k e d u c a t i o n c o m p a n y B e n c h m a r k e d u c a t i o n c o m p a n y ® ® BENCHMARK LITERACY OverviewTM Benchmark education company 629 Fifth Avenue • Pelham, NY • 10803 ©2014 Benchmark Education Company, LLC. All rights reserved. Teachers may photocopy the reproducible pages for classroom use. No other part of the guide may be reproduced or transmitted in whole or in part 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. ISBN: 978-1-4509-9670-9 For ordering information, call Toll-Free 1-877-236-2465 or visit our website at www.benchmarkeducation.com. BENCHMARK LITERACYTM Overview Common Core Edition Table of Contents Introducing Benchmark Literacy for Grades K–6 .
    [Show full text]
  • ESA Technology Programmes A
    ESA Technology Programmes A. Tobias European Space Agency Directorate of Technical and Quality Management January 2013 1. Strategic objectives and Technology The strategic objectives in the DG’s proposal to the 2012 Council at Ministerial level •Pushing the frontiers of knowledge Top class Science of space, in space and from Space •Enabling Services Earth observation, meteorology and environmental monitoring, navigation, telecommunications, space situation awareness, integrated applications •Supporting an innovative and competitive Europe 35 % of the satcom market, 50 % of launches to GTO, high multiplicative effort downstream, a sector of high gross added value, with high spin factor The keys: sustaining innovation, strengthening competitiveness and assuring a robust supply chain, and it all •Enabled by technology •Made possible by a competitive industry built during decades of technology and industrial policies and public investments in shared assets 1 • • • • The domains when theytakeoveratTRL5/6fromtechnologypreparation lines Investments intechnologydevelopmentsarefurther continuedinprojects for industry’scompetitivenessintheworldmarket investments inmissions/launchersspaceinfrastructures developmentsand 350 Exploration (Exomars),EarthObservation(MTG,MetOpSG,GSC) areas, orstabilizationinareaswithmajormissionprogrammes,e.g.Robotic Funding fortechnologydevelopmentwithanincreasingtrendinnearlyall Successful CM12,10B The programmes 2. ESATechnologyProgrammes 2. ESATechnologyProgrammes – 400 M € / yearintechnologydevelopmentlinesprepare3B
    [Show full text]
  • Space Situational Awareness
    → SPACE SITUATIONAL AWARENESS OUTLINE - Background - Purpose - Aims - Composition - Space Surveillance (SST) - Space Weather (SWE) - Near-Earth Objects (NEO) - Summary 2 BACKGROUND Image: Dan Durda – FIAAA 3 INTRODUCTION PURPOSE OF THE SSA PROGRAMME “The objective of the Space Situational Awareness (SSA) programme is to support the European independent utilisation of, and access to, space for research or services, through the provision of timely and quality data, information, services and knowledge regarding the space environment, the threats and the sustainable exploitation of the outer space surrounding our planet Earth.” - ESA Ministerial Council November 2008 4 INTRODUCTION AIMS OF THE SSA PROGRAMME • Independent utilisation of Space – Space assets are critical assets • Guarantee access to Space – Diplomatic, – Political – Regulatory – Technical • Serve EU “Lisbon Objectives” – New Applications – New Jobs – New Markets 5 INTRODUCTION CUSTOMERS FOR SSA SERVICES • European Governments • Space Insurance • United Nations – EU • Space Industry • Defence – National • Energy • Civil Protection – Regional – Surveying • European Space Agencies – Electrical Grid – ESA – Power Supply – National • Network Operations • Spacecraft Operators • Telecommunications – Commercial • Air Traffic Control – Academic • Search and Rescue Entities – Governmental 6 INTRODUCTION Current Objectives 2009 – 2012 • Preparatory Programme – Governance Definition – Data Policy – Architecture – Federation – Precursor Services – Radar Breadboard – Pilot Data Centres 2012
    [Show full text]
  • DLR Developments and Application Ideas for Interplanetary Cubesats
    DLR developments and application ideas for interplanetary cubesats iCubeSat, Milano 2019 Jens Biele1, Michael Maibaum1, Caroline Lange2, Thimo Grundmann2, Stephan Ulamec1, Marcus Thomas Knopp3, Frank-Cyrus Roshani3 1DLR German Aerospace Center, RB-MUSC, Cologne, Germany 2DLR German Aerospace Center, Bremen, Germany 3DLR German Aerospace Center, GSOC, Munich, Germany www.DLR.de • Chart 3 > Lecture > Author • Document > Date SKAD-Study [FRANK, MARCUS] • Orbiter as relais station for Mars-Rover • ………. Designs flown or studied (DLR) Hopper(10-25 kg) MASCOT (30, 70 kg) Philae (100 kg) Leonard MASCOT (10 kg) Folie 4 > Vortrag > Autor Folie 5 > Vortrag > Autor Study Flow of MASCOT („how to shrink a lander..“) • December 2008 – September 2009: feasibility study, with CNES, in context of Marco Polo and Hayabusa-2, with common requirements: • 3 iterations of different mass (95kg, 35kg & 10kg) and P/L • Settled on 10 kg lander package including 3 kg of P/L • Ho, T.-M., et al. (2016). "MASCOT—The Mobile Asteroid Surface Scout Onboard the Hayabusa2 Mission." Space Science Reviews 208(1-4): 339– 374. • ➔ Design of MASCOT 10 kg: a nanosat (30x30*20 cm³) . Could be a 18 U cubesat! Large ~ 95 kg, Philae hertitage Middle ~ 35 kg, Xtra Small ~ 10 kg, No post-landing Up-righting + mobility mobility MASCOT Payload (25% of total mass!) Instrument Science Goals Heritage Institute; PI/IM Mass [kg] MAG magnetization of the NEA MAG of ROMAP on Rosetta TU Braunschweig Lander (Philae), ESA VEX, 0,15 → formation history Themis K.H. Glassmeier / U. Auster mineralogical composition ESA ExoMars, Russia and characterize grains Phobos GRUNT, ESA size and structure of Rosetta, ESA ExoMars IAS Paris µOmega surface soil samples at μ- rover 2018, Rosetta / Philae J.P.
    [Show full text]
  • Marathon 2,500 Years Edited by Christopher Carey & Michael Edwards
    MARATHON 2,500 YEARS EDITED BY CHRISTOPHER CAREY & MICHAEL EDWARDS INSTITUTE OF CLASSICAL STUDIES SCHOOL OF ADVANCED STUDY UNIVERSITY OF LONDON MARATHON – 2,500 YEARS BULLETIN OF THE INSTITUTE OF CLASSICAL STUDIES SUPPLEMENT 124 DIRECTOR & GENERAL EDITOR: JOHN NORTH DIRECTOR OF PUBLICATIONS: RICHARD SIMPSON MARATHON – 2,500 YEARS PROCEEDINGS OF THE MARATHON CONFERENCE 2010 EDITED BY CHRISTOPHER CAREY & MICHAEL EDWARDS INSTITUTE OF CLASSICAL STUDIES SCHOOL OF ADVANCED STUDY UNIVERSITY OF LONDON 2013 The cover image shows Persian warriors at Ishtar Gate, from before the fourth century BC. Pergamon Museum/Vorderasiatisches Museum, Berlin. Photo Mohammed Shamma (2003). Used under CC‐BY terms. All rights reserved. This PDF edition published in 2019 First published in print in 2013 This book is published under a Creative Commons Attribution-NonCommercial- NoDerivatives (CC-BY-NC-ND 4.0) license. More information regarding CC licenses is available at http://creativecommons.org/licenses/ Available to download free at http://www.humanities-digital-library.org ISBN: 978-1-905670-81-9 (2019 PDF edition) DOI: 10.14296/1019.9781905670819 ISBN: 978-1-905670-52-9 (2013 paperback edition) ©2013 Institute of Classical Studies, University of London The right of contributors to be identified as the authors of the work published here has been asserted by them in accordance with the Copyright, Designs and Patents Act 1988. Designed and typeset at the Institute of Classical Studies TABLE OF CONTENTS Introductory note 1 P. J. Rhodes The battle of Marathon and modern scholarship 3 Christopher Pelling Herodotus’ Marathon 23 Peter Krentz Marathon and the development of the exclusive hoplite phalanx 35 Andrej Petrovic The battle of Marathon in pre-Herodotean sources: on Marathon verse-inscriptions (IG I3 503/504; Seg Lvi 430) 45 V.
    [Show full text]
  • Nagy Commentary on Euripides, Herakles
    Informal Commentary on Euripides, Herakles by Gregory Nagy 97 The idea of returning from Hades implies a return from death 109f The mourning swan... Cf. the theme of the swansong. Cf. 692ff. 113 “The phantom of a dream”: cf. skias onar in Pindar Pythian 8. 131f “their father’s spirit flashing from their eyes”: beautiful rendition! 145f Herakles’ hoped-for return from Hades is equated with a return from death, with resurrection; see 297, where this theme becomes even more overt; also 427ff. 150 Herakles as the aristos man: not that he is regularly described in this drama as the best of all humans, not only of the “Greeks” (also at 183, 209). See also the note on 1306. 160 The description of the bow as “a coward’s weapon” is relevant to the Odysseus theme in the Odyssey 203 sôzein to sôma ‘save the body’... This expression seems traditional: if so, it may support the argument of some linguists that sôma ‘body’ is derived from sôzô ‘save’. By metonymy, the process of saving may extend to the organism that is destined to be saved. 270 The use of kleos in the wording of the chorus seems to refer to the name of Herakles; similarly in the wording of Megara at 288 and 290. Compare the notes on 1334 and 1369. 297 See at 145f above. Cf. the theme of Herakles’ wrestling with Thanatos in Euripides Alcestis. 342ff Note the god-hero antagonism as expressed by Amphitryon. His claim that he was superior to Zeus in aretê brings out the meaning of ‘striving’ in aretê (as a nomen actionis derived from arnumai; cf.
    [Show full text]
  • The Pancam Instrument for the Exomars Rover
    ASTROBIOLOGY ExoMars Rover Mission Volume 17, Numbers 6 and 7, 2017 Mary Ann Liebert, Inc. DOI: 10.1089/ast.2016.1548 The PanCam Instrument for the ExoMars Rover A.J. Coates,1,2 R. Jaumann,3 A.D. Griffiths,1,2 C.E. Leff,1,2 N. Schmitz,3 J.-L. Josset,4 G. Paar,5 M. Gunn,6 E. Hauber,3 C.R. Cousins,7 R.E. Cross,6 P. Grindrod,2,8 J.C. Bridges,9 M. Balme,10 S. Gupta,11 I.A. Crawford,2,8 P. Irwin,12 R. Stabbins,1,2 D. Tirsch,3 J.L. Vago,13 T. Theodorou,1,2 M. Caballo-Perucha,5 G.R. Osinski,14 and the PanCam Team Abstract The scientific objectives of the ExoMars rover are designed to answer several key questions in the search for life on Mars. In particular, the unique subsurface drill will address some of these, such as the possible existence and stability of subsurface organics. PanCam will establish the surface geological and morphological context for the mission, working in collaboration with other context instruments. Here, we describe the PanCam scientific objectives in geology, atmospheric science, and 3-D vision. We discuss the design of PanCam, which includes a stereo pair of Wide Angle Cameras (WACs), each of which has an 11-position filter wheel and a High Resolution Camera (HRC) for high-resolution investigations of rock texture at a distance. The cameras and electronics are housed in an optical bench that provides the mechanical interface to the rover mast and a planetary protection barrier.
    [Show full text]
  • Hesiod Theogony.Pdf
    Hesiod (8th or 7th c. BC, composed in Greek) The Homeric epics, the Iliad and the Odyssey, are probably slightly earlier than Hesiod’s two surviving poems, the Works and Days and the Theogony. Yet in many ways Hesiod is the more important author for the study of Greek mythology. While Homer treats cer- tain aspects of the saga of the Trojan War, he makes no attempt at treating myth more generally. He often includes short digressions and tantalizes us with hints of a broader tra- dition, but much of this remains obscure. Hesiod, by contrast, sought in his Theogony to give a connected account of the creation of the universe. For the study of myth he is im- portant precisely because his is the oldest surviving attempt to treat systematically the mythical tradition from the first gods down to the great heroes. Also unlike the legendary Homer, Hesiod is for us an historical figure and a real per- sonality. His Works and Days contains a great deal of autobiographical information, in- cluding his birthplace (Ascra in Boiotia), where his father had come from (Cyme in Asia Minor), and the name of his brother (Perses), with whom he had a dispute that was the inspiration for composing the Works and Days. His exact date cannot be determined with precision, but there is general agreement that he lived in the 8th century or perhaps the early 7th century BC. His life, therefore, was approximately contemporaneous with the beginning of alphabetic writing in the Greek world. Although we do not know whether Hesiod himself employed this new invention in composing his poems, we can be certain that it was soon used to record and pass them on.
    [Show full text]
  • Dr. Sergei Fedorovich Teselkin Lavochkin Association, Russian Federation, [email protected]
    69th International Astronautical Congress 2018 Paper ID: 44581 oral IAF SPACE EXPLORATION SYMPOSIUM (A3) Solar System Exploration (5) Author: Dr. Sergei Fedorovich Teselkin Lavochkin Association, Russian Federation, [email protected] \TO VENUS TOGETHER": RUSSIAN-AMERICAN JOINT ENCORE OF VENUS RESEARCHES WITH ORBITER, LANDER AND ATMOSPHERIC PROBES IN THE PROJECT \VENUS-D" Abstract S. Lemeshevskii, Candidate of Economics, [email protected] O. Grafodatskiy, Doctor of Engineering Sci- ence,[email protected] Kh.Karchaev, Candidate of Economics, [email protected] S. Teselkin, Candi- date of PhysicsMathematics,[email protected] V. Vorontsov, Doctor of Engineering Science, [email protected] Lavochkin Association, Russia Mission "Venera-D" by Lavochkin Association implies a long-term study of Venus. International pay- load is to be installed on orbiter, lander and long-living station on Venus surface. The project is a basis for further large-scale international missions to Venus, previously carried out in 1960-80s and early 1990s by Soviet and American spacecraft. A large amount of data on structure, soil composition, atmosphere, cloud layers, wind speed on the surface were accumulated. Soviet Venus research program was completed in 1986 by landing of \VEGA" (Venus-Halley's comet), one of the most successful projects in Lavochkin history. Since 1994 (mapping with the NASA Magellan mission) Venus was studied by two spacecraft: \Venus Express" (ESA, 2005-2014) and \Akatsuki" (JAXA, launch - 2010, start of operation - 2015). The first steps of \Venera-D" appeared in the early 2000s with the idea to provide operations on the planet's surface for several hours and possibly days. With the latest developments, unification of design solutions and new technical tools used in-house Lavochkin experts consider the mission \VEGA" as a prototype for the next automatic interplanetary station destined to Venus.
    [Show full text]
  • First Woman Named Director of Jackson's Public Works Department
    www.mississippilink.com Vol. 20, No. 40 July 31 - August 6, 2014 50¢ Congratulations to winners of ... The 36th Mississippi The 40th Jackson Gospel Music Awards & Music Awards First woman James Brown biopic “Get named director of On Up!” filmed in Mississippi Jackson’s Public premieres in Jackson area By Stephanie R. Jones Contributing Writer Works Department Movie director Tate Taylor once again brought the glitz of Hollywood to Mississippi with a special premiere show- Kishia L. Powell’s city council ing of his latest project, the confirmation passes 5 yeas 1 abstention James Brown biopic “Get On Up!” By Ayesha K. Mustafaa About 575 attended the tick- Editor eted Sunday show at Malco Grandview in Madison, Miss., The Jackson City Council Sunday, July 27, 2014, to see held a confirmation hearing and greet movie stars as they in the public council meeting walked the red carpet, leading Tuesday, July 29, accepting up to a nationwide opening of with five yeas and one ab- the film on Friday, August 1. stention Mayor Tony Yarber’s The charity fundraiser took selection of Kishia L. Powell, in $30,000 for Mission Mis- Gov. Phil Bryant with wife Deborah, Tate Taylor, director of Get On Up! and Chadwick Boseman who P.E., as the director of the sissippi, an organization that portrays James Brown in the movie are all smiles at the movie premiere. PHOTO BY JAY JOHNSON city’s Public Works Depart- promotes racial reconcilia- ment., making her the first tion through the teachings of New York, but because it was “our visionary.” ter.
    [Show full text]
  • 2004-118.Pdf
    East MeetsWest in Near-Earth The Hubble Space Telescope Space SpaceTechnologies for Building Making the Most of Earth Observation Data The Hubble Space Telescope ESA's Cooperation with International Partners - Present and Future - Export Control lssues Nino Panagia Andre Farand & Ukike Bohlmann 49 ESA Reaches Out into Deep Space from Spain lntellectual Property Rights -The New Cebreros Station - A New Regime in ESA Contracts Valeriano Claros, Gisela Siiss & Manfred Warhaut tt Karl Eisermann & Christian Grafd 55 East Meets West in Near-Earth Space Programmes in Progress bU - Double Star Bodo Gramkow et al. z.t News - In Brief 76 Making the Most of Earth Observation with Publications 82 Data Assimilation Alan O'Neill, Pierre-Philippe Mathieu & Claus Zehner JJ Space Technologies for the Building Sector Fritz Gamoe 41 eso bulletin ll8-moy 2004 For over twenty yeors Gore Spoce Wire ond Cobies hcve contributed to the success of mony spoce missions, slch os Moon Londing, Spcceob, EURECA, ERSI + 2, lfolsol, SAX, SPCT, lSC, Envisot, XMM, Metop, Integrol, scienfific reseorch in spoce, Co,.lmbus As o speciol cob e supplier we support you in p onning the nexf sfep inlo spoce Coll us now. EORE IEI + 49/91 44/6 Al O Creative Technologies FAX.+ 49/91 44/6a l4 53 Worldwide e ectronics europe@w gore com www goree ecfron co com Our spoce communicotion scenqrio covers the whole ronge of sotellite ond spocecroh opplicotions: Telecommunicotions, Eorth Observotion, Science, Spoce Inlrostructure ond Novigotion. As on experienced developer & supplier of On-Boord TTC & Doto Tronsmission, Pqssive Microwoves, Digitol Processing Units. For over fifteen yeors, Alcotel Espocio hos contributed to the success of more thon 50 progroms sotellites Alcotel Espocio is o Sponish subsidiory compony of Alcotel Spoce BROADEN YOUR IIFE Nino Panogio Spoce Telexope Srience Inslilule, ISA Direclorole of Scientific Progrommes, Boltimore, USA Hubble role in n of the mosl importonl ond prolilic spoce oslronomy nissions of oll time.
    [Show full text]
  • Planetary Protection at ESA Issues & Status
    Planetary Protection at ESA Issues & Status Gerhard Kminek Planetary Protection Officer, ESA NASA Planetary Protection Subcommittee Meeting 12-13 November 2013, GSFC Selected Missions BepiColombo → Launch of a composite spacecraft, comprising the MTM, the MPO and MMO on an Ariane V from CSG; nominal launch slot opens July 2016 → Planetary Protection Category II, due to Venus gravity assist → Launcher upper stage and spacecraft impact on Mars analysis described and agreed during CDR Solar Orbiter → Launch of the spacecraft on a NASA provided launch vehicle from KSC; nominal launch is 2017 → Planetary Protection Category II, due to Venus gravity assist → Spacecraft probability of Mars impact demonstrated to be within requirement → Scope for the launcher upper stage probability of Mars impact discussed with NASA ExoMars → See later presentation Jupiter Icy Moon Explorer (JUICE) → Selected L-class mission in the frame of the Cosmic Vision Program → ESA lead mission to the Jovian system with focus on Ganymede and Europa → Launch planned on Ariane V from CSG in 2022 → Phase A completed; currently in PRR in preparation for Phase B → Planetary Protection Category III → Planetary protection approach for Europa agreed (probability of impact < 1x10-4) → Planetary protection approach for Ganymede will be reviewed based on a recently published paper during the next ESA PPWG Candidate Missions Phootprint → Mission candidate in the frame of the Mars Robotic Exploration Preparatory (MREP) Program for launch opportunities from 2024 onwards → ESA lead mission to return samples from the martian moon Phobos → Launch planned on Ariane V from CSG with a return to Woomera Test Range, Australia → Planetary Protection Category V, unrestricted Earth return (to be confirmed) → Dedicated activity initiated to evaluate the level of assurance that no unsterilized martian material naturally transferred to Phobos is accessible to a Phobos sample return mission; result will be published in a peer reviewed journal, reviewed by a panel organised by the ESF, incl.
    [Show full text]