BepiColombo. Project and MPO Status. Comprehensive Explora1on of Planet Mercury
|
|
- Francis McKinney
- 5 years ago
- Views:
Transcription
1 BepiColombo Project and MPO Status Comprehensive Explora1on of Planet Mercury
2 Joe Zender BepiColombo Deputy PS, ESA/ESTEC BepiColombo Previously: Ø Proba2 Science Coordinator, until 12/2013 Ø ProbaV, Project Office Member, until 12/2013 Ø Rosetta, (PT) LSS Support, in 2014, then Proba3, PS, from 01/2015 (tbc) Ø BC Deputy PS (PT), from 01/2014
3 Guide through the talk Orbit Update in 2013 Mission CDR in 2013 Development Status as of today
4 critical issue orbit As a consequence of gravity field measurements by MESSENGER the orbit needed to be updated MPO MMO Date (MJD2000) hp (km) ha (km) T(h) i( ) Ω( ) ω( ) Table 1: Initial orbital elements of MPO and MMO in the Mercury equatorial system.
5 BC SWT RESOLUTION on new orbit (3 rd September 2013) On September 3, 2013, updated MPO and MMO science orbits were proposed by the project to the BC-SWT, taking into account the impact of the most recent updates of the gravitational parameters of Mercury. The SWT makes the following statements regarding the new proposed orbits of MPO (480*1500km) and MMO (590*11639km, south pole orbit insertion): Both proposed orbits are acceptable to obtain the science goals of the mission and can be used for spacecraft and science analysis. Future adaptations of the MPO orbit - in particular to secure a lower than 400km periherm altitude during the mission - shall be possible within the given constraints (thermal, delta_v). Given the current uncertainty in the gravity field of Mercury, the SWT will revisit this issue once updated MESSENGER data are available.
6 Periherm altitude change over time Periherm altitude [km] Time [days] Figure 1: MPO periherm altitude profile over 800 days.
7 Apoherm Altitude change over time Apoherm altitude [km] Time [days] Figure 2: MPO apoherm altitude profile over 800 days.
8 Mission Design Critical Design Review ü Board Meeting held on 15 Nov 13 CDR closed ü Number of major issues identified as below è Solar array substrate manufacturing and test è Survival Mode duration in superior conjunction è Survivability of an Aphelion eclipse in case of no MMO separation è Limited ground visibility with MPO in survival mode è Schedule leading to launch date of July 2016 è Micro Vibration acceptability è DSN network availability
9 Rocket: ARIANE 5 ECA Launch: July 2016 Start of Science Mission: 2024 Total Launch mass: 4200 Kg
10 Launch Opportunities è Launch July 2016: baseline, maintained since CDR with repeating opportunities in January 2017, July 2017 Arrival January 2024 (1 Earth, 2 Venus and 5 Mercury fly-bys)
11 BepiColombo Status (May 2014)
12 Project Status MPO PFM unit and payload final integration in Torino (Italy) ALL P/L TC sequences, required for System Function Test, have been finalized and debugged. Shipment to ESTEC planned for week 32 The MTM PFM integration for thermal and chemical propulsion hardware is on-going. Shipment to ESTEC planned for week 32 (tbc) MMO FM integration and functional verification is finished The mission and science operations preparation activities proceed as planned. CDR at Project Level planned for November 2014, including spacecraft (ESA,JAXA), payload, launcher, and ground segment
13 Mercury Planetary Orbiter: Status ü Harness integration complete ü All instruments integrated and IST completed; ü All AOCS units except wheels integrated and tested ü All data handling and power units integrated ü 22 N thrusters integrated and tested ü 5 N thrusters integrated and tested
14 Mercury Transfer Module: Status Chemical Propellant Subsystem equipment integrated Proof and leak test of high pressure section of propulsion subsystems performed System harness integration completed SEPS harness and first SEPS elements to come in July14; coupling test 2 running nominally
15 Contamination progress achieved Updated Model of instrument molecular contamination (MOC) established demonstrates that instrument MOC requirements achievable with implementation of protection measures è Protection measures (e.g. MLI Gap closures, Collars around apertures) under implementation è Decisions on equipment bake-out taken after justification and impact assessment è MMO/MOSIF Protective Foil agreed, detailed design under implementation Ongoing activities Cleanliness WG continues to follow-up remaining actions Test programme and materials defined for effects of UV/VUV; first tests running in ESTEC; completion expected mid 2015
16 Launcher ü HSS3+ low-shock fairing separation system successfully demonstrated on ATV-4 launch of Ariane 5 ü HSS3+ formally offered by Arianespace for BC è adopted as project baseline ü Retires all pending risks of re-qualification of MPO/MTM equipment Ariane 5 ECA delta-qualification in preparation
17 Project Status Summary ü Critical issues identified during CDR under control ü BC Schedule quite stable since 1 year ü BC TBTV test in autumn 2014 ü All P/L (replacement) models for MPO TBTV test available è Additional exchange slot for P/L end 2013 è Remaining FM P/L delivery trends critical
18 Spacecraft Performance
19 Spacecraft limitations è impact on BC science performance? 1. Science Data Return 2. Power Budget for science operations 3. Thermal Design 4. Pointing Constraints 5. Mass / reachable Science Orbit
20 Science data return (REQ: 1550 Gbits) The data volume per year varies 1381 Gbits (-10% for no power sharing operation and nominal sun activity) 1250 Gbits (-15% Ka-Band DL switched-off for 15 days and maximum sun activity) è Shortcomings on science return data volume have a tremendous impact on the science return of BepiColombo. Major science goals will not be achievable è problems can be solved (mitigate, compensate) by additional data download of about 300 Gbit via an additional/another ground station
21 Power Availability (REQ: ~160 Watt) è Outside Ground Station contact at Perihelion most instruments can be operated è During Ground Station contact at Perihelion most instruments cannot operating. This equates to a loss of about 35% of the science operation time at perihelion (~6% total). è Shortcomings on Power Availability during Perihelion Phase will impact the science return
22 Thermal Design issues Illustration of P/L Restriction due to Thermal Constraints
23 Thermal Design non-compliances è Further case studies/analysis are necessary current data base is insufficient to make proper scientific performance evaluation è Details analysis involving instrument teams/sgs of realistic scenarios is needed (to what limit can an instrument team tolerate design limit violations; what kind of margins are needed, etc è Thermal design shortcomings will lead to a major science degradation during perihelion (+/- 5-7days)
24 Pointing Performance Remaining non-compliances for: HRIC & STC which is driven by the AOCS performance, which is 10.9 arcsec based on worst case calculation assumption and calibration strategy BELA is non-compliant, because it can not be calibrated (provides values similar to other non-calibrated instruments) Note: Values given are worst case. For Nadir pointing results for SIMBIO-SYS are about a factor 2 better!!
25 critical issue Pointing Micro Vibration acceptability - Non-compliances in pointing and micro-vibration: - SIMBIO-SYS: è to be mitigated with specific calibration activities measures to determine thermal distortion effects - closed - BELA: è an improved analysis was delivered to the team and discussed and agreed - closed - ISA:è micro-vibration non-compliance under further evaluation - open
26 Mass Budget Negative overall MPO Mass Budget (-38kg) will lead to a degraded MPO science orbit Note: 1670km instead 1500km (-1kg = 4.5km orbit delta height) this value is a worst case prediction taken all uncertainties about outstanding units not yet delivered and accepted into account. However, it is still possible to reach nominal apoherm distance (Margin on MPO items 31.2kg). Depletion of AOGS margin would lead to improvement of ~60km) è Shortcomings on mass may be compensated
27 NEXT SWT Meeting SWT2014 Place: Tokyo, Japan Dates: Sep Organizers: Ichiro Yoshikawa (U Tokyo) Shingo Kameda (Rikkyo U)
28 The BepiColombo Mission Thank you!
BepiColombo Project Status. Presentation for MESSENGER Science Team Meeting Via-Skype, 27 th March 2015
BepiColombo Project Status Johannes.Benkhoff@esa.int Presentation for MESSENGER Science Team Meeting Via-Skype, 27 th March 2015 Project status The purpose of this presentation is to give an overview on
More informationBepiColombo Mission to Mercury - コロンボ. October Jan van Casteren, Mauro Novara.
ベピ - コロンボ BepiColombo Mission to Mercury October 2010 Jan van Casteren, Mauro Novara http://www.esa.int/science/bepicolombo June 2010 1 BepiColombo Scientific Objectives Origin and evolution of a planet
More informationAn Overview of BepiColombo Thermal Analysis
An Overview of BepiColombo Thermal Analysis Presented by Ian Renouf, Astrium UK ESTEC 9-10 th Summary About BepiColombo Thermal Design Issues Required Thermal Analysis Thermal Modelling Issues Proposed
More informationBepiColombo MPO Science Operations Planning Drivers IWPSS-2013
BepiColombo MPO Science Operations Planning Drivers IWPSS-2013 Sara de la Fuente sfuente@sciops.esa.int BepiColombo MPO Science Ground Segment ESA, ESAC, Villanueva de la Cañada, Madrid, 28691, Spain Summary
More informationESA UNCLASSIFIED For Official Use. BepiColombo à Exploring Mercury
BepiColombo à Exploring Mercury ESA / JAXA BepiColombo Mercury Mercury has always been something of a puzzle for planetary scientists. Its close position to the Sun means it is very difficult to observe.
More informationSOLAR FURNACE. By Heiko Ritter JOURNEY TO THE INNER
SOLAR FURNACE 88 Seite 1 By Heiko Ritter JOURNEY TO THE INNER THERMAL TESTS FOR Seite 2 SOLAR SYSTEM B E P I C O L O M B O T he European Space Agency, ESA, is currently developing a mission to the planet
More informationThermal Correlation of BepiColombo MOSIF 10 Solar Constants Simulation Test. Savino De Palo Tiziano Malosti (ThalesAlenia Space, Italy)
271 Appendix Q Thermal Correlation of BepiColombo MOSIF 10 Solar Constants Simulation Test Savino De Palo Tiziano Malosti (ThalesAlenia Space, Italy) Gianluca Filiddani (Sofiter System Eng., Italy) 272
More informationFeasible Mission Designs for Solar Probe Plus to Launch in 2015, 2016, 2017, or November 19, 2008
Feasible Mission Designs for Solar Probe Plus to Launch in 2015, 2016, 2017, or 2018 2007 Solar Probe Study & Mission Requirements Trajectory study and mission design trades were conducted in the fall
More informationSP-1291 June Mars Express. The Scientific Investigations
SP-1291 June 2009 Mars Express The Scientific Investigations Operations and Archiving Mars Express Science Planning and Operations R. Pischel & T. Zegers ESA/ESTEC, Research and Scientific Support Department,
More informationBepiColombo Mission to Mercury
BepiColombo Mission to Mercury Updates Mission & MPO Payload Scientific Objectives Origin and evolution of a planet close to the parent star Mercury as a planet: form, interior, geology, composition Origin
More informationScience planning and operations for Mars Express
Science planning and operations for Mars Express René Pischel and Tanja Zegers ESA/ESTEC, Research and Scientific Support Department, Postbus 299, 2200 AG Noordwijk, The Netherlands I. Introduction The
More informationEnd of Life Re-orbiting The Meteosat-5 Experience
End of Life Re-orbiting The Meteosat-5 Experience Milan EUMETSAT, Darmstadt, Germany This article illustrates the orbit maneuver sequence performed during Meteosat- 5 End of Life (EOL) re-orbiting operations
More informationBUILDING LOW-COST NANO-SATELLITES: THE IMPORTANCE OF A PROPER ENVIRONMENTAL TESTS CAMPAIGN. Jose Sergio Almeida INPE (Brazil)
BUILDING LOW-COST NANO-SATELLITES: THE IMPORTANCE OF A PROPER ENVIRONMENTAL TESTS CAMPAIGN Jose Sergio Almeida INPE (Brazil) 1 st International Academy of Astronautics Latin American Symposium on Small
More informationPlanetary 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
More informationMISSION ENGINEERING SPACECRAFT DESIGN
MISSION ENGINEERING & SPACECRAFT DESIGN Alpbach 2007 - D.J.P. Moura - CNES MISSION ENGINEERING (1) OVERALL MISSION ENGINEERING IS A COMPLEX TASK SINCE AT THE BEGINNING THE PROBLEM IS GENERALLY BADLY EXPRESSED
More informationThe radio science experiment with BepiColombo mission to Mercury
Mem. S.A.It. Vol. 87, 24 c SAIt 2016 Memorie della The radio science experiment with BepiColombo mission to Mercury G. Schettino 1, S. Di Ruzza 2, F. De Marchi 1, S. Cicalò 2, G. Tommei 1, and A. Milani
More informationSpace mission environments: sources for loading and structural requirements
Space structures Space mission environments: sources for loading and structural requirements Prof. P. Gaudenzi Università di Roma La Sapienza, Rome Italy paolo.gaudenzi@uniroma1.it 1 THE STRUCTURAL SYSTEM
More informationTRAJECTORY DESIGN OF SOLAR ORBITER
TRAJECTORY DESIGN OF SOLAR ORBITER José Manuel Sánchez Pérez ESA-ESOC HSO-GFA, Robert-Bosch-Str., Darmstadt, 293, Germany, 9--929, jose.manuel.sanchez.perez@esa.int Abstract: In the context of the ESA
More informationPlanning Drivers for the BepiColombo MPO Science Payload Operations
Planning Drivers for the BepiColombo MPO Science Payload Operations Sara de la Fuente 1, Raymond Hoofs 2, Mauro Casale 3 BepiColombo MPO Science Ground Segment ESA, ESAC, Villanueva de la Cañada, Madrid,
More informationSpectroscopy for planetary upper atmospheres きょくたん
Spectroscopy for planetary upper atmospheres きょくたん Spectrum of Venus atmosphere Spectrum of Jupiter and Io Figure 1. An EUV spectrum measured by Hisaki spacecraft. The spectrograph mixes spatial and spectral
More informationAppendix C. Mercury Retro-Reflection Modelling and Effects on MPO Solar Array. Anja Frey Giulio Tonellotto (ESA/ESTEC, The Netherlands)
51 Appendix C Mercury Retro-Reflection Modelling and Effects on MPO Solar Array Anja Frey Giulio Tonellotto (ESA/ESTEC, The Netherlands) 9 th European Space Thermal Analysis Workshop 3 November 15 5 Mercury
More informationHerschel Mission Overview and Key Programmes
Herschel Mission Overview and Key Programmes SPIE Astronomical Instrumentation 2008 Space Telescopes and Instrumentation I: Optical, Infrared, and Millimeter Wave Marseille, 23-28 June 2008 Göran L. Pilbratt
More informationMercury radio science experiment of the mission BepiColombo
Mem. S.A.It. Suppl. Vol. 20, 127 c SAIt 2012 Memorie della Supplementi Mercury radio science experiment of the mission BepiColombo A. Genova, M. Marabucci, and L. Iess Dipartimento di Inegneria Meccanica
More informationIMPACT OF SPACE DEBRIS MITIGATION REQUIREMENTS ON THE MISSION DESIGN OF ESA SPACECRAFT
IMPACT OF SPACE DEBRIS MITIGATION REQUIREMENTS ON THE MISSION DESIGN OF ESA SPACECRAFT Rüdiger Jehn (1), Florian Renk (1) (1 ) European Space Operations Centre, Robert-Bosch-Str. 5, 64293 Darmstadt, Germany,
More informationThe time period while the spacecraft is in transit to lunar orbit shall be used to verify the functionality of the spacecraft.
ASE 379L Group #2: Homework #4 James Carlson Due: Feb. 15, 2008 Henri Kjellberg Leah Olson Emily Svrcek Requirements The spacecraft shall be launched to Earth orbit using a launch vehicle selected by the
More informationESA activities towards the Gravitation Waves Space Observatory
ESA activities towards the Gravitation Waves Space Observatory Frédéric Safa ESA Science Directorate, Future Missions LISA Symposium, Zurich 2016 The Gravitation Wave Observatory in ESA Science Programme
More informationPROBA 1. F. Teston ESA/ESTEC D/TEC-EL
PROBA 1 F. Teston ESA/ESTEC D/TEC-EL Frederic.Teston@esa.int PROBA 1 launch PROBA 1 has been launched on 21 October 2001 Orbital parameters: Altitude: 681-561 km Near polar (inclination of 97.9 ) Sun-synchronous
More informationSolar Orbiter Ballistic Transfer Mission Analysis Synthesis
European Space Agency Agence Spatiale Européenne directorate of operations and infrastructure ground systems engineering department mission analysis office MAO Working Paper No. 483 Issue 1, Rev. 0 Solar
More informationMission Overview. EAGLE: Study Goals. EAGLE: Science Goals. Mission Architecture Overview
Mission Overview OPAG Meeting November 8 th, 2006 Ryan Anderson & Daniel Calvo EAGLE: Study Goals Develop a set of science goals for a flagship mission to Enceladus Investigate mission architectures that
More informationISAS MERCURY ORBITER MISSION TRAJECTORY DESIGN STRATEGY. Hiroshi Yamakawa
ISAS MERCURY ORBITER MISSION TRAJECTORY DESIGN STRATEGY Hiroshi Yamakawa Institute of Space and Astronautical Science (ISAS) 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-851 Japan E-mail:yamakawa@pub.isas.ac.jp
More informationOverview of the Current Baseline of the Solar-C Spacecraft System
Overview of the Current Baseline of the Solar-C Spacecraft System Keisuke YOSHIHARA (JAXA) 11 November, 2013 Solar-C Science Meeting Hida Earth Wisdom Center, Takayama, Japan Solar-C Spacecraft System
More informationSmall Satellite Aerocapture for Increased Mass Delivered to Venus and Beyond
Small Satellite Aerocapture for Increased Mass Delivered to Venus and Beyond Adam Nelessen / Alex Austin / Joshua Ravich / Bill Strauss NASA Jet Propulsion Laboratory Ethiraj Venkatapathy / Robin Beck
More informationUpdate on the In-orbit Performances of GIOVE Clocks
Update on the In-orbit Performances of GIOVE Clocks Pierre Waller, Francisco Gonzalez, Stefano Binda, ESA/ESTEC Ilaria Sesia, Patrizia Tavella, INRiM Irene Hidalgo, Guillermo Tobias, GMV Abstract The Galileo
More informationThe Quantum Sensor Challenge Designing a System for a Space Mission. Astrid Heske European Space Agency The Netherlands
The Quantum Sensor Challenge Designing a System for a Space Mission Astrid Heske European Space Agency The Netherlands Rencontres de Moriond - Gravitation, La Thuile, 2017 Quantum Sensors in Lab Experiments
More informationESA Heliophysics missions
ESA Heliophysics missions C. Philippe Escoubet ESA/ESTEC With help from J. Benkhoff, B. Fleck, D. Mueller, M. Taylor, J. Zender ESA Heliophysics Missions In operations - SOHO - Hinode - Cluster - Proba
More informationOverview of the Jovian Exploration Technology Reference Studies
Overview of the Jovian Exploration Technology Reference Studies The Challenge of Jovian System Exploration Peter Falkner & Alessandro Atzei Solar System Exploration Studies Section ESA/ESTEC Peter.Falkner@esa.int,
More informationCAS-ESA Call for small mission proposals - Technical annex
CAS-ESA Call for small mission proposals - Technical annex Copenhagen workshop 23/09/2014 Table of contents 1. General considerations Mass & power Schedule Work breakdown and share Technology readiness
More informationMission Design Options for Solar-C Plan-A
Solar-C Science Definition Meeting Nov. 18, 2008, ISAS Mission Design Options for Solar-C Plan-A Y. Kawakatsu (JAXA) M. Morimoto (JAXA) J. A. Atchison (Cornell U.) J. Kawaguchi (JAXA) 1 Introduction 2
More informationSeminar BELA STAR SIMULATOR
Seminar BELA STAR SIMULATOR Sumita Chakraborty, Michael Affolter, Jakob Neubert (external contractor), Stefan Graf, Daniele Piazza and many more Universität Bern Content > Mercury > BepiColombo > MPO and
More informationVenus Express: Results, Status and Future Plans
Venus Express: Results, Status and Future Plans Håkan Svedhem ESA/ESTEC Present Status The spacecraft and its payload in general is in a good condition, with the following remarks: One of the two coolers
More informationSELENE TRANSLUNAR TRAJECTORY AND LUNAR ORBIT INJECTION
SELENE TRANSLUNAR TRAJECTORY AND LUNAR ORBIT INJECTION Yasuihiro Kawakatsu (*1) Ken Nakajima (*2), Masahiro Ogasawara (*3), Yutaka Kaneko (*1), Yoshisada Takizawa (*1) (*1) National Space Development Agency
More informationThe Solar System in the ESA scientific program
The Solar System in the ESA scientific program 1 ESA-ESTEC/SRE-SM, Postbus 299 2200 AG Noordwijk (The Netherlands) Tel: +31-71 565 3573 Fax: +31-71 565 4697 luigi.colangeli@esa.int Luigi Colangeli Head,
More informationStatus of the European Student Moon Orbiter (ESMO) Project:
Status of the European Student Moon Orbiter (ESMO) Project: Roger Walker, Project Manager Education Projects Unit, ESA Education Office, ESTEC 1 What is ESMO? Fourth mission in the ESA Education Satellite
More informationSpace Debris Mitigation Activities at ESA in 2013
Space Debris Mitigation Activities at ESA in 2013 Heiner Klinkrad ESA Space Debris Office H. Klinkrad (ESA) 51st UNCOPUOS STSC 14-Feb-2014 page 1 ESA Launches in 2013 PROBA-V (2013-021A) launch May 7,
More informationOrbit Design Marcelo Suárez. 6th Science Meeting; Seattle, WA, USA July 2010
Orbit Design Marcelo Suárez Orbit Design Requirements The following Science Requirements provided drivers for Orbit Design: Global Coverage: the entire extent (100%) of the ice-free ocean surface to at
More informationPredicting Long-Term Telemetry Behavior for Lunar Orbiting, Deep Space, Planetary and Earth Orbiting Satellites
Predicting Long-Term Telemetry Behavior for Lunar Orbiting, Deep Space, Planetary and Earth Orbiting Satellites Item Type text; Proceedings Authors Losik, Len Publisher International Foundation for Telemetering
More informationJUpiter Icy Moons Explorer (JUICE) Status report for OPAG. N. Altobelli (on behalf of O. Witasse) JUICE artist impression (Credits ESA, AOES)
JUpiter Icy Moons Explorer (JUICE) Status report for OPAG N. Altobelli (on behalf of O. Witasse) JUICE artist impression (Credits ESA, AOES) Message on behalf of the JUICE Science Working Team Congratulations
More informationRESERVE THALES ALENIA SPACE CHANGE RECORDS ISSUE DATE DESCRIPTION OF CHANGES AUTHOR
ISSUE : 1 Page : 2/35 CHANGE RECORDS ISSUE DATE DESCRIPTION OF CHANGES AUTHOR 1 03/10/07 Initial issue (MTG-TAF-SA-RS-39) J. VIEILLOT 1 20/09/10 Updated version for kick off : L.OUCHET New reference (MTG-TAF-SA-SS-0039)
More informationCosmic Ray Telescope for the Effects of Radiation to Spacecraft Thermal Interface Control Document
Effective Date: February 14, 2006 Expiration Date: February 14, 2011 Lunar Reconnaissance Orbiter Project Cosmic Ray Telescope for the Effects of Radiation to Spacecraft Thermal Interface Control Document
More informationESMO Mission Analysis
Changing the economics of space ESMO Mission Analysis SRR Workshop Alison Gibbings 22 nd 26 th March 2010 Review of the existing baseline Sensitivity analysis Contents At lunar Injection Along the WSB-Moon
More informationMechanical and Thermal Design of XMM
r bulletin 100 december 1999 Mechanical and Thermal Design of XMM K. van Katwijk, T. van der Laan & D. Stramaccioni XMM Project, ESA Directorate for Scientific Programmes, ESTEC, Noordwijk, The Netherlands
More informationDARE Mission and Spacecraft Overview
DARE Mission and Spacecraft Overview October 6, 2010 Lisa Hardaway, PhD Mike Weiss, Scott Mitchell, Susan Borutzki, John Iacometti, Grant Helling The information contained herein is the private property
More informationJUICE/Laplace Mission Summary & Status
JUICE/Laplace Mission Summary & Status C. Erd JUICE Instrument WS, Darmstadt 9/11/2011 Activities during the Reformulation Phase 1. Feasible JGO s/c as a starting point a. no re-design of s/c necessary
More informationReport of the Venera-D Joint Science Definition Team: "Together to Venus"
Report of the Venera-D Joint Science Definition Team: "Together to Venus" L. Zasova1, D. Senske2, T. Economou3, N. Eismont1, L. Esposito4, M. Gerasimov1, N. Ignatiev1, M. Ivanov5, I. Khatuntsev1, O. Korablev1,
More informationBINARY ASTEROID ORBIT MODIFICATION
2013 IAA PLANETARY DEFENSE CONFERENCE BEAST BINARY ASTEROID ORBIT MODIFICATION Property of GMV All rights reserved TABLE OF CONTENTS 1. Mission Concept 2. Asteroid Selection 3. Physical Principles 4. Space
More informationROSETTA. One Comet Rendezvous and two Asteroid Fly-bys. Rita Schulz Rosetta Project Scientist
ROSETTA One Comet Rendezvous and two Asteroid Fly-bys Rita Schulz Rosetta Project Scientist Giotto Mission 1986 1P/Halley DS-1 Mission 2001 19P/Borrelly Stardust Mission 2004 81P/ Wild 2 Deep Impact Mission
More informationNumerical analysis of the compliance of interplanetary CubeSats with planetary protection requirements
Numerical analysis of the compliance of interplanetary CubeSats with planetary protection requirements Francesca Letizia, Camilla Colombo University of Southampton 5th Interplanetary CubeSat Workshop Session
More informationLRO/CRaTER. Technical Interchange Meeting. LRO Mechanical Systems. Giulio Rosanova / /
LRO/CRaTER Technical Interchange Meeting LRO Mechanical Systems Giulio Rosanova / 543 301-286-5907 / Giulio.G.Rosanova@nasa.gov 1 LRO Baseline (Deployed 0n Orbit) High Gain Antenna IM Optical Bench /Radiator
More informationMAE 180A: Spacecraft Guidance I, Summer 2009 Homework 4 Due Thursday, July 30.
MAE 180A: Spacecraft Guidance I, Summer 2009 Homework 4 Due Thursday, July 30. Guidelines: Please turn in a neat and clean homework that gives all the formulae that you have used as well as details that
More informationYour Partner in Environment Monitoring
Your Partner in Environment Monitoring Radiation Environment in Space The ionizing radiation in space represents one of the most severe environmental loads to space hardware and can cause a large number
More informationILWS Update April 2005
CLUSTER Space Plasma Missions in the Science Programme of ESA ILWS Update April 2005 Hermann J. Opgenoorth ESA ESTEC Solar and Solar Terrestrial Missions Division (SCI-SH) Research and Scientific Support
More informationLOTNAV. A Low-Thrust Interplanetary Navigation Tool: The Trajectory Reconstruction Module
LOTNAV A Low-Thrust Interplanetary Navigation Tool: The Trajectory Reconstruction Module Juan Luis Cano González Mission Analysis Division Deimos Space S.L. -1- The LOTNAV Tool The Low-Thrust Interplanetary
More informationAndrea Sainati, Anupam Parihar, Stephen Kwan Seklam 31 A Very Low Altitude Constellation For Earth Observation
Andrea Sainati, Anupam Parihar, Stephen Kwan Seklam 31 A Very Low Altitude Constellation For Earth Observation Andrea Sainati, Anupam Parihar, Stephen Kwan Seklam MSc students, Department of Aerospace
More informationNASA s Planetary Science Program Status
NASA s Planetary Science Program Status Presentation to VEXAG James L. Green Director, Planetary Science Division October 28, 2009 1 Outline MSL status Announcements of Opportunity R&A International Agreements
More informationHayabusa Status and Proximity Operation. As of September 2nd, 2005
Hayabusa Status and Proximity Operation As of September 2nd, 2005 2005/9/2 0 What is Hayabusa? World s First Round-trip Interplanetary Flight HAYABUSA Challenge to Asteroid Sample Return Touch-down + Dimensions
More informationTeam X Study Summary for ASMCS Theia. Jet Propulsion Laboratory, California Institute of Technology. with contributions from the Theia Team
Team X Study Summary for ASMCS Theia Jet Propulsion Laboratory, California Institute of Technology with contributions from the Theia Team P. Douglas Lisman, NASA Jet Propulsion Laboratory David Spergel,
More informationThe Interstellar Boundary Explorer (IBEX) Mission Design: A Pegasus Class Mission to a High Energy Orbit
The Interstellar Boundary Explorer (IBEX) Mission Design: A Pegasus Class Mission to a High Energy Orbit Ryan Tyler, D.J. McComas, Howard Runge, John Scherrer, Mark Tapley 1 IBEX Science Requirements IBEX
More informationDE-ORBITATION STUDIES AND OPERATIONS FOR SPIRALE GTO SATELLITES
DE-ORBITATION STUDIES AND OPERATIONS FOR SPIRALE GTO SATELLITES François BONAVENTURE (1), Slim LOCOCHE (2), Anne-Hélène GICQUEL (3) (1) Tel. (+33) (0)5 62 19 74 27, E-mail. francois.bonaventure@astrium.eads.net
More informationSuccessful Demonstration for Upper Stage Controlled Re-entry Experiment by H-IIB Launch Vehicle
11 Successful Demonstration for Upper Stage Controlled Re-entry Experiment by H-IIB Launch Vehicle KAZUO TAKASE *1 MASANORI TSUBOI *2 SHIGERU MORI *3 KIYOSHI KOBAYASHI *3 The space debris created by launch
More informationFLIGHT DYNAMICS MISSION ANALYSIS AND OPERATIONS FOR GALILEO SATELLITES: ORBITAL MANEUVERS STRATEGY DESIGN AND PERFORMANCES
FLIGHT DYNAMICS MISSION ANALYSIS AND OPERATIONS FOR GALILEO SATELLITES: ORBITAL MANEUVERS STRATEGY DESIGN AND PERFORMANCES Angélique Gaudel (1), Denis Carbonne (2), Pierre Labourdette (3), Laurence Lorda
More informationASTEROID IMPACT MISSION: AIM3P MISSION AND PAYLOAD OPERATIONS SCENARIO
estec European Space Research and Technology Centre Keplerlaan 1 2201 AZ Noordwijk The Netherlands T +31 (0)71 565 6565 F +31 (0)71 565 6040 www.esa.int ASTEROID IMPACT MISSION: AIM3P MISSION AND PAYLOAD
More information483 Lecture. Space Mission Requirements. February11, Definition Examples Dos/ Don ts Traceability
483 Lecture Space Mission February11, 2012 Photo Credit:: http://www.spacewallpapers.info/cool-space-wallpaper What s a Requirement? ification? Requirement A concept independent statement of a mix of needs,
More informationLAUNCH SYSTEMS. Col. John Keesee. 5 September 2003
LAUNCH SYSTEMS Col. John Keesee 5 September 2003 Outline Launch systems characteristics Launch systems selection process Spacecraft design envelope & environments. Each student will Lesson Objectives Understand
More informationSciBox, a Proven Automated Planning and Commanding System
SciBox, a Proven Automated Planning and Commanding System Teck Choo, Edward Russell, Michael Kim February 25, 2014 2014 by The Johns Hopkins University/Applied Physics Laboratory. Published by The Aerospace
More informationESWT 10 Mission Systems Design and Schedule
ESWT 10 Mission Systems Design and Schedule 1 EXoMars 2020 International Cooperation 2 Project industry organization ESA Inter-Agency agreement Steering coordination ROSCOSMOS ESA ExoM Project Project
More informationNewsletter of the INTEGRAL Science Operations Centre
Newsletter of the INTEGRAL Science Operations Centre No. 4 January 2002 Foreword Christoph Winkler - Project Scientist Status of spacecraft and payload Astrid Orr - Operations Scientist During the past
More informationVenus Express Aerobraking and End of Mission
Venus Express Aerobraking and End of Mission Håkan Svedhem ESA/ESTEC Pericentre velocity vs Orbital Period Examples (VEX): Delta-V needed for Reduction of orbital period: 24h-18h 90m/s 18h-16h 42m/s 18h-12h
More informationCosmic Ray Telescope for the Effects of Radiation to Spacecraft Thermal Interface Control Document
Effective Date: 01/11/2007 Expiration Date: 01/11/2012 Lunar Reconnaissance Orbiter Project Cosmic Ray Telescope for the Effects of Radiation to Spacecraft Thermal Interface Control Document December 19,
More informationFlight Demonstration of Electrostatic Thruster Under Micro-Gravity
Flight Demonstration of Electrostatic Thruster Under Micro-Gravity Shin SATORI*, Hiroyuki MAE**, Hiroyuki OKAMOTO**, Ted Mitsuteru SUGIKI**, Yoshinori AOKI # and Atsushi NAGATA # * Hokkaido Institute of
More informationHigh Power Electric Propulsion Pointing Mechanisms (HP EPPM) Technical Development Activities (TDA s) strategy, status and planning
High Power Electric Propulsion Pointing Mechanisms (HP EPPM) Technical Development Activities (TDA s) strategy, status and planning Objectives of this presentation are: To provide primes with: ESA preliminary
More informationNovember 3, 2014 Eric P. Smith JWST Program Office
November 3, 014 Eric P. Smith JWST Program Office 1 SINCE LAST CAA MEETING... Completed of 3 recommended GAO schedule risk analyses for this year. Mutually agreed to drop 3 rd. Will perform cost-risk study
More informationVenus Express: The Spacecraft
Venus Express: The Spacecraft Venus Express Spacecraft Alistair J. Winton, Ared Schnorhk, Con McCarthy, Michael Witting, Philippe Sivac, Hans Eggel, Joseph Pereira, Marco Verna Venus Express Project Team,
More informationNew Worlds Observer Operations Concept NEW WORLDS OBSERVER OPERATIONS CONCEPT (OPSCON)
NEW WORLDS OBSERVER OPERATIONS CONCEPT (OPSCON) 1 Table of Contents 1.0 Mission Overview... 1 1.1 NWO scope... 1 2.0 System Overview... 2 2.1 System constituents... 2 2.2 system functional architecture...
More informationBepiColombo SWT # October 2017, Matera
BepiColombo SWT #16 23 27 October 2017, Matera Hotel San Domenico al Piano Via Roma 15 - Matera (Italy) 23 October 2017 9:15 Participant welcome 9:30 BepiColombo HEWG splinter agenda see below 18:00 End
More informationMission analysis forms an integral
Artist s impression of ESA s Mars Sample Return orbiter vehicle. This mission presents many mission analysis challenges Mission Analysis Johannes Schoenmaekers, Rüdiger Jehn, Markus Landgraf & Michael
More informationUSA Space Debris Environment, Operations, and Policy Updates
USA Space Debris Environment, Operations, and Policy Updates Presentation to the 48 th Session of the Scientific and Technical Subcommittee Committee on the Peaceful Uses of Outer Space United Nations
More informationarxiv:gr-qc/ v1 15 Nov 2004
Mission design for LISA Pathfinder arxiv:gr-qc/0411071v1 15 Nov 2004 M Landgraf, M Hechler, and S Kemble ESA/ESOC, Robert-Bosch-Straße 5, D-64293 Darmstadt, Germany E-mail: Markus.Landgraf@esa.int EADS
More informationESA s Juice: Mission Summary and Fact Sheet
ESA s Juice: Mission Summary and Fact Sheet JUICE - JUpiter ICy moons Explorer - is the first large-class mission in ESA's Cosmic Vision 2015-2025 programme. Planned for launch in 2022 and arrival at Jupiter
More informationGOES-R Instrument Status and Accommodations. Barbara Pfarr GOES-R Program Systems Engineering January 2010 AMS Conference
GOES-R Instrument Status and Accommodations Barbara Pfarr GOES-R Program Systems Engineering January 2010 AMS Conference Agenda Instrument Developmental Status Significant Changes in the Last Year Introducing
More informationFigure 1. View of ALSAT-2A spacecraft
ALSAT-2A TRANSFER AND FIRST YEAR OPERATIONS M. Kameche (1), A.H. Gicquel (2), D. Joalland (3) (1) CTS/ASAL, 1 Avenue de la Palestine, BP 13, Arzew 31200 Oran, Algérie, email:mo_kameche@netcourrier.com
More informationDRAFT. Robotic Lunar Exploration Program Lunar Reconnaissance Orbiter (LRO)
DRAFT Robotic Lunar Exploration Program Lunar Reconnaissance Orbiter (LRO) Comic Ray Telescope for the Effects of Radiation (CRaTER) to Spacecraft Mechanical Interface Control Document Date: July 13, 2005
More informationFlight Operations Preparation for the BepiColombo Mission to Mercury: Concepts and Challenges
SpaceOps Conferences 16-20 May 2016, Daejeon, Korea SpaceOps 2016 Conference 10.2514/6.2016-2485 Flight Operations Preparation for the BepiColombo Mission to Mercury: Concepts and Challenges Christoph
More informationSun Shield. Solar Paddle
The Institute of Space and Astronautical Science Report SP No.14, December 2000 Current Status of ASTRO-F By Hiroshi Murakami Λ (November 1, 2000) Abstract: The ASTRO-F is the second infrared astronomy
More informationTechnology Reference Studies
In the proceedings of the 8th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2004' ESTEC, Noordwijk, The Netherlands, November 2-4, 2004 Technology Reference Studies P.
More informationDRAFT. Robotic Lunar Exploration Program Lunar Reconnaissance Orbiter 431-ICD Date: September 15, 2005
DRAFT Robotic Lunar Exploration Program Lunar Reconnaissance Orbiter Lunar Reconnaissance Orbiter to Comic Ray Telescope for the Effects of Radiation Mechanical Interface Control Document Date: September
More informationASTOS for Low Thrust Mission Analysis
ASTOS for Low Thrust Mission Analysis 3rd Astrodynamics Workshop, Oct. 26, ESTEC Overview Low Thrust Trajectory Computation Description of the Optimal Control Problem Trajectory Optimization and Mission
More informationSmall Satellite Aerocapture for Increased Mass Delivered to Venus and Beyond
Small Satellite Aerocapture for Increased Mass Delivered to Venus and Beyond Adam Nelessen / Alex Austin / Joshua Ravich / Bill Strauss NASA Jet Propulsion Laboratory Ethiraj Venkatapathy / Robin Beck
More informationSTATUS OF THE JUICE MISSION
STATUS OF THE JUICE MISSION D. Titov, O. Witasse, N. Altobelli, G. Sarri, Ph. Gare, C. Erd JUICE Science Team ESA Project Team JUICE artist impression (Credits ESA, AOES) JUICE: JUpiter Icy moons Explorer
More informationAsteroid Impact Mission (AIM)
Asteroid Impact Mission (AIM) Andrés Gálvez, ESA HQ, Paris, France Ian Carnelli, ESA HQ, Paris, France Carlos Corral, ESTEC, Noordwijk, The Netherlands & the AIDA team (JHU/APL, NASA, OCA. DLR) NEO mission
More informationOrbiter Element Brian Cooke
Orbiter Element Brian Cooke 47 from orbit Payload focused primarily to address Ocean objective: Radio Subsystem (RS) Laser Altimeter (LA) Magnetometer (MAG) Langmuir Probe (LP) Mapping Camera (MC) Have
More information