Technology Reference Studies
|
|
|
- Hollie Simpson
- 5 years ago
- Views:
Transcription
1 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. Falkner A. Lyngvi, M.L. van den Berg, D. Renton, A. Atzei and A. Peacock Dr. ASTRA WS2004, ESTEC, Nov 04 Page 1
2 Outline Technology Reference Studies (TRS) Background Venus Entry Probe (VEP) Deimos Sample Return (DSR) Jupiter Explorer Mission (JEM) Interstellar Heliopause Probe (IHP) Relevance for Robotics Conclusion Dr. ASTRA WS2004, ESTEC, Nov 04 Page 2
3 Background Strategic focus on critical technology developments for potential future science missions Study technologically demanding, science driven missions that are not part of the science program Identifying critical technologies to enable future missions Establishing a roadmap for technology developments (e.g. TRP2/GSTP4 technology plan) Enable low resource exploration missions Assist the community and ESA in future proposal submission and assessment Enable new low-cost science mission scenarios at increased frequency Provide focus and references for technology development Provide technology in time Dr. ASTRA WS2004, ESTEC, Nov 04 Page 3
4 Current Technology Reference Studies Venus Entry Probe (VEP) Deimos Sample Return (DSR) Jovian Minisat Explorer (JME) Interstellar Heliopause Probe (IHP) Solar Polar Orbiter (SPO) Dedicated talk at ASTRA 2004 Atomic Interferometer X-ray Interferometer Gamma Ray Imager Selection Process: Selected to serve with a small number of TRSs a wide application range DSR small gravity environment, docking & rendezvous, re-entry,.. JEM High radiation, long distance (communication & power supply) VEP Aerobot, Microprobes, localisation & communication, IHP Nuclear power, autonomy, lifetime, solar sails Dr. ASTRA WS2004, ESTEC, Nov 04 Page 4
5 Technology Reference Studies Top-level assumptions: Small launcher, low cost typical Soyuz-Fregat class Use of MicroSat or MiniSat Enable more frequent & phased approaches Based on Highly Integrated Payload Suites Use of Centralised Processing and Power Supply Based on resource reduction and optimisation (Payload and S/C-subsystems) Designed to low cost Dr. ASTRA WS2004, ESTEC, Nov 04 Page 5
6 Venus Entry Probe Detailed in-situ & remote study of the Venus atmosphere Origin and evolution of Venus atmosphere Comparative planetology Composition of lower atmosphere Atmospheric chemistry Greenhouse effect Tracking active volcanism Aerosol analysis/exobiology Analysis of large (ø ~ 7 µm) cloud particles Atmospheric dynamics Super-rotation Hadley cell circulation? Weather patterns in main cloud deck Polar vortices Dr. ASTRA WS2004, ESTEC, Nov 04 Page 6
7 Venus Entry Probe Launch by Soyuz-Fregat 2-1B from Kourou Earth escape, 150 days transfer VEP Two MiniSat s: Low Venus Orbiter - LVO orbit: km x km, inclination = 90 Remote sensing atmospheric investigations concurrent with aerobot Dry mass: 258 kg VRS LVO Venus Relay Satellite VRS orbit: 250 km x 7500 km, inclination = 75 to 90 Deploys entry probe from HEO (250 km x km) Studies ionosphere and (sub)-surface Dry mass: 450 kg Long duration aerobot (VEP) Global in-situ atmospheric coverage Atmospheric microprobes (VMP) Vertical profiles of p, T, flux, wind velocity VRS SF-2B Fairing Dr. ASTRA WS2004, ESTEC, Nov 04 Page 7
8 Venus Entry Probe Key Technological Challenges Aerobot Atmospheric entry Balloon material Gas storage Survivability in Venus atmosphere (~14 days) Miniaturized payload Miniaturized power source 200 g acceleration Atmospheric Microprobes Localization and communication Aero-thermodynamic design Miniaturized payload Sub-system integration See session :00h 3-Nov Dr. ASTRA WS2004, ESTEC, Nov 04 Page 8
9 Small Body Sample Return to Deimos AIM To study and develop the technology required to return a 1kg sample of Deimos Regolith back to Earth Dr. ASTRA WS2004, ESTEC, Nov 04 Page 9
10 Deimos Sample Return 1. Launch into a 200 x km HEO Earth orbit on a Soyuz-Fregat 2B 2. Earth-Mars Transfer 3. Mars Orbit Insertion to 500 x km orbit 4. Mars Orbit Maneuvers to enter into a co-orbit with Deimos ( km circular orbit) Earth Departure Mars-Deimos Operations 5. Sample Collection Maneuvers 6. Mars Orbit Maneuvers to return to 500 x km orbit 7. Mars-Earth Transfer 8. Earth Entry Vehicle (EEV) performs Direct Re-Entry Dr. ASTRA WS2004, ESTEC, Nov 04 Page 10
11 Sampling Method: Preliminary Proposal Obtain Sample quickly and efficiently from the homogeneous regolith on Deimos surface Optimize sampling method for a small, low gravity body Touch-and-Go Sampling Sampling will require high precision control Operations will require high autonomy due to communication lag time Highly Autonomous Guidance, Navigation and Control System Dr. ASTRA WS2004, ESTEC, Nov 04 Page 11
12 Earth Entry Vehicle (EEV) door bandage bio-shield Sample door bio-shield separation mechanism s Provides break in contamination chain Performs direct Re-Entry Protects against contamination on Impact (must survive a hard landing) Contains a beacon for localization and recovery after impact Mass ~ 50 kg Dr. ASTRA WS2004, ESTEC, Nov 04 Page 12
13 Deimos Sample Return Key Technological Challenges Low Gravity Sample Return Sample Mechanism Obtain a sample from a low gravity body Obtain a sample in a short time frame (few seconds) Highly Autonomous Micro GNC System Perform delicate sampling maneuvers Earth Re-Entry Capsule Perform Earth direct entry Safely land in designed zone Planetary Protection Guidelines Dr. ASTRA WS2004, ESTEC, Nov 04 Page 13
14 Jupiter Minisat Explorer Scientific goals: Study the Jovian environment (e.g. radiation, magnetic field) Jupiter s moons, especially Europa: study the global topography (surface features, including recent or current activity) study the composition of the (sub)surface mapping of the ice thickness is a subsurface ocean present? Dr. ASTRA WS2004, ESTEC, Nov 04 Page 14
15 Jupiter Minisat Explorer Launch with Soyuz-Fregat Jupiter transfer Venus-Earth-Earth Gravity Assist Transfer duration: 6 years Solar cell based power system Two satellite configuration: 1. JEO (Europa Orbiter) 200 km circular polar orbit achieved after > 1 year tour science phase duration: maximum of ~60 days 2. JRS (Data Relay S/C): Highly elliptical polar Jupiter orbit Avoiding Radiation Belts Jupiter Dr. ASTRA WS2004, ESTEC, Nov 04 Page 15
16 Jupiter Minisat Explorer Mass budget JRS (kg) JEO (kg) Jupiter Relay Sat Power AOCS 8 8 Propulsion CMDS Communications Structure Thermal 10 6 Radiation shielding 8 27 Total Soyuz Fregat 2B launch Europa Orbiter Launch Date Total DV (m/s) Duration (yrs) 19-Jul Jul Apr Oct Jan Jun Feb May Oct Aug Nov Dr. ASTRA WS2004, ESTEC, Nov 04 Page 16
17 Jupiter Minisat Explorer Key Technological Challenges Development of low resource deep space minisats Deep space as well as Jupiter s extreme radiation environment: Radiation hardened components ( ( 1 Mrad) + radiation shielding Radiation optimised solar cells (LILT), development required Development of highly integrated systems (especially low resource radar) Maximize the use of solar power, even at ~5 AU from Sun Low power deep space communication Planetary protection compatible systems Microprobe System A low cost series of missions to explore the Jovian system in a phased strategic approach is realistic Dr. ASTRA WS2004, ESTEC, Nov 04 Page 17
18 Interstellar Heliopause Probe Scientific objective: Explore and investigate the interface between the local interstellar medium and the heliosphere IHP Investigate the nature of the interstellar medium Investigate how the interstellar medium affect the solar system Investigate how the solar system impact the interstellar medium Technologies for IHP are of great benefit for Outer Planet missions Dr. ASTRA WS2004, ESTEC, Nov 04 Page 18
19 Interstellar Heliopause Probe Soyuz Fregat 2B launch Solar sail mission with a=1 mm/s 2 Close approach to the Sun R=0.25AU Jettison sail at 5 AU Reach 200 AU in 25 years Dr. ASTRA WS2004, ESTEC, Nov 04 Page 19
20 Strawman payload Instrument Mass (kg) Power (W) Plasma analyser 2 1 Plasma and radio wave experiment Magnetometer Neutral and charged atom detector Energetic particle detector Dust analyser UV-photometer CPU+CPS Structures 2 - Total (incl. 20 % system margin) Dr. ASTRA WS2004, ESTEC, Nov 04 Page 20
21 Current Spacecraft Configuration System Mass (kg) Science instruments 22 Attitude Determination and Control 35 Telemetry, tracking and command 61 On-board data handling 12 Thermal Control 14 Power 42 Mechanisms and structure 27 Total mass 213 Sail System mass will be approximately kg Total launch mass: kg including 20 % system margin Dr. ASTRA WS2004, ESTEC, Nov 04 Page 21
22 Interstellar Heliopause Probe Key Technological Challenges Solar Sail: Deployment system of large structures > m 2 Very large, thin and light sail film < 2 µm Light boom structures < 100 g/m ADCS Sail jettison mechanism S/C bus Radioisotope power (specific power of ~ 10 W/kg) Deep space communication (Optical vs. RF) Lifetime and Autonomy Dr. ASTRA WS2004, ESTEC, Nov 04 Page 22
23 Conclusions TRS: Selected to provide references for Solar System Exploration Provides realistic set of Requirements for Technology Development Several Technologies already identified ESA Technology Programme Aim: Provide Technology for Science Missions in time High relevance for robotics and automation Need serious funding Dr. ASTRA WS2004, ESTEC, Nov 04 Page 23
Overview 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,
SCI-AP Preprints October 2004
SCI-AP Preprints October 2004 Recent papers related to studies initiated by the Planetary Explorations Studies Section of the Science Payloads and Advanced Concepts Office International Astronautical Congress
Robotic Lunar Exploration Scenario JAXA Plan
Workshop May, 2006 Robotic Lunar Exploration Scenario JAXA Plan Tatsuaki HASHIMOTO JAXA 1 Question: What is Space Exploration? Answers: There are as many answers as the number of the people who answer
ESA s (future) Science Mission Overview
ESA s (future) Science Mission Overview P. Falkner,, Science Direcrate, European Space Agency Peter.Falkner@esa.int / phone: +3 7 565 5363 P. Falkner Science Missions @ ASTRA WS 28Nov 2006, ESTEC Page
ESA 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
THE INTERSTELLAR HELIOPAUSE PROBE
THE INTERSTELLAR HELIOPAUSE PROBE A. Lyngvi 1, P. Falkner 1, S. Kemble 2, M. Leipold 3 and A. Peacock 1 1 Science Payloads & Advanced Concepts Office, European Space Agency, ESTEC, The Netherlands 2 EADS
JUICE/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
ESA Robotic Science Missions Overview
10 th ASTRA WS ESA Robotic Science Missions Overview P. Falkner, European Space Agency 10 th ASTRA Workshop, ESTEC, 11. Nov. 2008 1 Contents Science Missions Overview Focus Future CV missions Exploration
JUICE: A European Mission to Jupiter and its Icy Moons. Claire Vallat Prague, 15 th November 2018
JUICE: A European Mission to Jupiter and its Icy Moons Claire Vallat Prague, 15 th November 2018 Emergence of habitable worlds around the gas giants The Jupiter icy moons family portrait [Lammer et al,
SOLAR ORBITER Linking the Sun and Inner Heliosphere. Daniel Müller
SOLAR ORBITER Linking the Sun and Inner Heliosphere Outline Science goals of Solar Orbiter Focus of HELEX joint mission Mission requirements Science payload Status update Top level scientific goals of
Solar Sailing as an Enabling Technology
Dr. Eur Ing Malcolm Macdonald 22 April 2009 at the European Week of Astronomy and Space Science Solar Sailing as an Enabling Technology www.strath.ac.uk/space malcolm.macdonald.102@strath.ac.uk Overview
SCIENCE WITH DIRECTED AERIAL DR. ALEXEY PANKINE GLOBAL AEROSPACE CORPORATION SAILING THE PLANETS
: SCIENCE WITH DIRECTED AERIAL ROBOT EXPLORERS (DARE) DR. ALEXEY PANKINE GLOBAL AEROSPACE CORPORATION 1 NEW ARCHITECTURE FOR PLANETARY EXPLORATION KEY ELEMENTS: Long-Duration Planetary Balloon Platforms
SAILING THE PLANETS: PLANETARY EXPLORATION FROM GUIDED BALLOONS. 7 th Annual Meeting of the NASA Institute for Advanced Concepts
SAILING THE PLANETS: PLANETARY EXPLORATION FROM GUIDED BALLOONS 7 th Annual Meeting of the NASA Institute for Advanced Concepts DR. ALEXEY PANKINE GLOBAL AEROSPACE CORPORATION SAILING THE PLANETS 1 MARS
Formation Flying and Rendezvous and Docking Simulator for Exploration Missions (FAMOS-V2)
Formation Flying and Rendezvous and Docking Simulator for Exploration Missions (FAMOS-V2) Galder Bengoa, F. Alonso, D. García, M. Graziano (GMV S.A.) Dr. Guillermo Ortega (ESA/ESTEC) 2nd ESA Workshop on
ESSE Payload Design. 1.2 Introduction to Space Missions
ESSE4360 - Payload Design 1.2 Introduction to Space Missions Earth, Moon, Mars, and Beyond Department of Earth and Space Science and Engineering Room 255, Petrie Science and Engineering Building Tel: 416-736
Last Class. Today s Class 11/28/2017
Today s Class: The Jovian Planets & Their Water Worlds 1. Exam #3 on Thursday, Nov. 30 th! a) Covers all the reading Nov. 2-28. b) Covers Homework #6 and #7. c) Review Space in the News articles/discussions.
Feasible 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
ASTRIUM. Interplanetary Path Early Design Tools at ASTRIUM Space Transportation. Nathalie DELATTRE ASTRIUM Space Transportation.
Interplanetary Path Early Design Tools at Space Transportation Nathalie DELATTRE Space Transportation Page 1 Interplanetary missions Prime approach: -ST has developed tools for all phases Launch from Earth
Interstellar Exploration Through Repeated External Acceleration
Interstellar Exploration Through Repeated External Acceleration Andrew Bingham NIAC Student Fellows Prize Department of Mechanical and Aeronautical Engineering, Clarkson University NIAC Fellows Meeting,
HERA MISSION & CM16 lessons learned
HERA MISSION HERA MISSION & CM16 lessons learned (CM16) Schedule criticality for 2020 launch Prepare Asteroid mission with launch opportunities in 2023 (with back-up in 2024 and 2025) (CM16) Payload selection
A Lander for Marco Polo
A Lander for Marco Polo Hermann Boehnhardt MPI for Solar System Research Katlenburg-Lindau, Germany Lutz Richter DLR, Institute for Space Systems Bremen, Germany The ROSETTA Lander PHILAE passive lander
STATUS 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
Expanding Science with SmallSats/CubeSats
National Aeronautics and Space Administration Expanding Science with SmallSats/CubeSats Outer Planets Analysis Group John D. Baker 2/2/2016 2016, Government Sponsorship Acknowledged National Aeronautics
Orbiter 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
Challenges to. Future Outer Heliosphere. and Interstellar Probes. Science. Mission. Technology,
Science Challenges to Mission Future Outer Heliosphere Technology, and Interstellar Probes TRL Robert F. Wimmer-Schweingruber wimmer@physik.uni-kiel.de Univ. Kiel, Germany on behalf of the IP Team http://www.ieap.uni-kiel.de/et/people/wimmer/ip
In situ Investigations of the Local Interstellar Medium. Science Mission Technology, TRL
Science Mission Technology, TRL 1 Introduction Astrospheres are a ubiquitous phenomenon... LL Orionis Visible Hubble Astrosphere: The region in space influenced by the outflowing stellar wind and embedded
Last Class. Jupiter. Today s Class
Today s Class: Jupiter & Its Waterworld Moons 1. Reading for Next Class: Saturn and its moons Chapter 11 in Cosmic Perspective. 2. Homework #8 will be due next Wednesday, April 18. 3. Need 2 more volunteers
Space Physics: Recent Advances and Near-term Challenge. Chi Wang. National Space Science Center, CAS
Space Physics: Recent Advances and Near-term Challenge Chi Wang National Space Science Center, CAS Feb.25, 2014 Contents Significant advances from the past decade Key scientific challenges Future missions
PLANET-C: Venus Climate Orbiter mission from Japan. Takeshi Imamura Japan Aerospace Exploration Agency PLANET-C team
PLANET-C: Venus Climate Orbiter mission from Japan Takeshi Imamura Japan Aerospace Exploration Agency PLANET-C team Venus Climate Orbiter JAXA s 24th science spacecraft dedicated to the exploration of
ESA s Cosmic Vision Programme: Outer Planet Mission Studies
ESA s Cosmic Vision Programme: Outer Planet Mission Studies Jean-Pierre LEBRETON (ESA s EJSM and TSSM Study Scientist) Europa Lander workshop IKI, Moscow, 9-13 February 2009 ESA/ESTEC, Noordwijk, Pays-Bas
Remote Imaging of Electron Acceleration at the Sun with a Lunar Radio Array
Remote Imaging of Electron Acceleration at the Sun with a Lunar Radio Array J. Kasper Harvard-Smithsonian Center for Astrophysics 6 October 2010 Robotic Science From the Moon: Gravitational Physics, Heliophysics
Jupiter Icy Moons Orbiter
Jupiter Icy Moons Orbiter Forum on Concepts and Approaches for Jupiter Icy Moons Orbiter Science Capabilities & Workshop Goals Dr. Colleen Hartman Director of Solar System Exploration June 12, 2003 the
INTERSTELLAR PRECURSOR MISSIONS USING ADVANCED DUAL-STAGE ION PROPULSION SYSTEMS
INTERSTELLAR PRECURSOR MISSIONS USING ADVANCED DUAL-STAGE ION PROPULSION SYSTEMS David G Fearn, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, UK dg.fearn@virgin.net Roger Walker Advanced
Design of Orbits and Spacecraft Systems Engineering. Scott Schoneman 13 November 03
Design of Orbits and Spacecraft Systems Engineering Scott Schoneman 13 November 03 Introduction Why did satellites or spacecraft in the space run in this orbit, not in that orbit? How do we design the
Toward Venus orbit insertion of Akatsuki
Toward Venus orbit insertion of Akatsuki Takeshi Imamura (JAXA, Japan) Lightning and Airglow Camera Mid-IR Camera UV Imager Ultra-Stable Oscillator 1µm Camera 2µm Camera Development and launch Objective:
Optimal Gravity Assisted Orbit Insertion for Europa Orbiter Mission
Optimal Gravity Assisted Orbit Insertion for Europa Orbiter Mission Deepak Gaur 1, M. S. Prasad 2 1 M. Tech. (Avionics), Amity Institute of Space Science and Technology, Amity University, Noida, U.P.,
Aeolus. A Mission to Map the Winds of Mars. Anthony Colaprete Amanda Cook NASA Ames Research Center
Aeolus A Mission to Map the Winds of Mars Anthony Colaprete Amanda Cook NASA Ames Research Center Low-Cost Planetary Missions Conference 12, 2017 What is Aeolus? Science Aeolus will provide the very first
HEOMD Overview March 16, 2015
National Aeronautics and Space Administration HEOMD Overview March 16, 2015 Ben Bussey Chief Exploration Scientist HEOMD, NASA HQ National Aeronautics and Space Administration NASA Strategic Plan Objective
The 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
Advanced Probes for Planetary Surface and Subsurface Exploration
Workshop on Space Robotics, ICRA 2011 Advanced Probes for Planetary Surface and Subsurface Exploration Takashi Kubota (JAXA/ISAS/JSPEC) Hayato Omori, Taro Nakamura (Chuo Univ.) JAXA Space Exploration Program
Toward Venus orbit insertion of Akatsuki
Toward Venus orbit insertion of Akatsuki Takeshi Imamura (JAXA, Japan) Lightning and Airglow Camera Mid-IR Camera UV Imager Ultra-Stable Oscillator 1µm Camera 2µm Camera Development and launch Objective:
Operational Aspects of Space Weather-Related Missions
Operational Aspects of Space Weather-Related Missions Richard G. Marsden, ESA/SCI-SH Outline SOHO: Example of Near-Earth Observatory-class Mission Ulysses: Example of Deep Space Monitor-class Mission Solar
JUpiter Icy Moons Explorer (JUICE) Status report for OPAG. O. Witasse and N. Altobelli. JUICE artist impression (Credits ESA, AOES)
JUpiter Icy Moons Explorer (JUICE) Status report for OPAG O. Witasse and N. Altobelli JUICE artist impression (Credits ESA, AOES) Jupiter Icy Moons Explorer MISSION SCIENCE (1/3) EXPLORATION OF HABITABLE
9 Aug 04 Getting Technology to Space for the Warfighter
1 SMC Detachment 12 - The Dirty Dozen Space Test Program-1 (STP-1) First of its Kind! Major Ray Galik STP-1 Program Manager 9 Aug 2004 Overview STP-1 Mission summary STP-1 Firsts Manifest Changes Space
JUpiter 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
Science Scenario Modeling
Science Scenario Modeling Rob Lock, Erick Sturm, Tracy Van Houten Presented to OPAG Satellite Break-out Group February 2010 Introduction Scenario Strategy For Europa Explorer and Jupiter Europa Orbiter
Introduction of Small Solar Power Sail Demonstrator IKAROS
Introduction of Small Solar Power Sail Demonstrator IKAROS IKAROS Demonstration Team JAXA Space Exploration Center (JSPEC) Japan Aerospace Exploration Agency (JAXA) Overview of IKAROS IKAROS is a space
JUICE: the first European mission to Jupiter and its Icy Moons
JUICE: the first European mission to Jupiter and its Icy Moons Giuseppe Sarri Knowledge Transfer Seminar @ CERN 26 April 2018 ESA UNCLASSIFIED - For Official Use European Space Agency (ESA) The European
January 11-12, 2007 VEXAG Meeting, Crystal City, VA
January 11-12, 2007 VEXAG Meeting, Crystal City, VA The Venus Exploration Analysis Group (VEXAG) was established by NASA in July 2005 to identify scientific priorities and strategy for exploration of Venus.
ESA VENUS ENTRY PROBE STUDY
Presented at the 2 nd International planetary probe workshop, Moffett Field, Ca USA, August 2004 ESA VENUS ENTRY PROBE STUDY M.L. van den Berg (1), P. Falkner (1), A. Phipps (2), J.C. Underwood (3), J.S.
Toshinori Kuwahara*, Yoshihiro Tomioka, Yuta Tanabe, Masato Fukuyama, Yuji Sakamoto, Kazuya Yoshida, Tohoku University, Japan
Toshinori Kuwahara*, Yoshihiro Tomioka, Yuta Tanabe, Masato Fukuyama, Yuji Sakamoto, Kazuya Yoshida, Tohoku University, Japan The 3 rd Nano-Satellite Symposium Micro/Nano Satellite & Debris Issues December
Comparative Planetology I: Our Solar System. Chapter Seven
Comparative Planetology I: Our Solar System Chapter Seven ASTR 111 003 Fall 2006 Lecture 07 Oct. 16, 2006 Introduction To Modern Astronomy I Introducing Astronomy (chap. 1-6) Planets and Moons (chap. 7-17)
Astrodynamics of Moving Asteroids
Astrodynamics of Moving Asteroids Damon Landau, Nathan Strange, Gregory Lantoine, Tim McElrath NASA-JPL/CalTech Copyright 2014 California Institute of Technology. Government sponsorship acknowledged. Capture
Solar 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
LOW-COST LUNAR COMMUNICATION AND NAVIGATION
LOW-COST LUNAR COMMUNICATION AND NAVIGATION Keric Hill, Jeffrey Parker, George H. Born, and Martin W. Lo Introduction Spacecraft in halo orbits near the Moon could relay communications for lunar missions
Europa Exploration: Challenges and Solutions
Europa Exploration: Challenges and Solutions T. V. Johnson 1, K. Clark 1, R. Greeley 2, R. Pappalardo 1,3 1 Jet Propulsion Laboratory, Pasadena, CA, 2 Arizona State University, Tempe AZ, 3 U. of Colorado,
JAXA s Venus Climate Orbiter (PLANET-C) overview. Launch: Jun 2010 Arrival: Dec 2010 Mission life: 2 years
JAXA s Venus Climate Orbiter (PLANET-C) overview Launch: Jun 2010 Arrival: Dec 2010 Mission life: 2 years Venus and Earth They have almost the same size and mass. Surface environments are completely different.
Deployment of an Interstellar Electromagnetic Acceleration System
Deployment of an Interstellar Electromagnetic Acceleration System Andrew Bingham Department of Mechanical and Aeronautical Engineering Clarkson University Phase I Fellows Meeting March 15-16, 2005 Atlanta,
Direct Aerial Robot Explorers (DARE) For Planetary Exploration
Direct Aerial Robot Explorers (DARE) For Planetary Exploration Presentation to NIAC Fellows Meeting By Dr. Alexey Pankine Global www.gaerospace.com Global October 23, 2002 CONTRIBUTORS Global Prof. Andrew
SURVEY OF THE ELECTRIC SOLAR WIND SAIL: THE FASTEST MAN-MADE DEVICE EVER BUILT
SURVEY OF THE ELECTRIC SOLAR WIND SAIL: THE FASTEST MAN-MADE DEVICE EVER BUILT Nick R. Purtle 1 University of Oklahoma, Norman, OK, 73069 In recent years, scientists have discovered that there are planets
Rocket Science, Reentry and the Race to Mars. From Science Fiction to Simulation
Rocket Science, Reentry and the Race to Mars From Science Fiction to Simulation Julian Köllermeier RWTH Aachen, November 1st 2015 The Mars half the diameter of the Earth 40% of Earth s gravity 2 moons
Radiation Environments, Effects and Needs for ESA Missions
Radiation Environments, Effects and Needs for ESA Missions Eamonn Daly European Space Agency ESTEC, Noordwijk, The Netherlands Space Environment Engineering and Science Applications Workshop 5 September
Orbit 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
Mars Atmosphere and Volatile Evolution Mission (MAVEN) Status of the MAVEN Mission at Mars 18 May 2018
Mars Atmosphere and Volatile Evolution Mission (MAVEN) Status of the MAVEN Mission at Mars 18 May 2018 Bruce Jakosky Laboratory for Atmospheric and Space Physics University of Colorado at Boulder USA MAVEN
Mission Analysis of Sample Return from Jovian Trojan Asteroid by Solar Power Sail
Trans. JSASS Aerospace Tech. Japan Vol. 12, No. ists29, pp. Pk_43-Pk_50, 2014 Original Paper Mission Analysis of Sample Return from Jovian Trojan Asteroid by Solar Power Sail By Jun MATSUMOTO 1), Ryu FUNASE
HERA MISSION. ESA UNCLASSIFIED - For Official Use
HERA MISSION ESA UNCLASSIFIED - For Official Use HERA/AIM mission scenario! First ever investigation of deflection test! Detailed analysis of impact crater (before/after impact or after only depending
Solution for Homework# 3. Chapter 5 : Review & Discussion
Solution for Homework# 3 Chapter 5 : Review & Discussion. The largest telescopes are reflecting telescopes, primarily because of 3 distinct disadvantages of the refracting telescope. When light passes
Space and Robotics. History of Unmanned Spacecraft David Wettergreen The Robotics Institute Carnegie Mellon University
Space and Robotics History of Unmanned Spacecraft David Wettergreen The Robotics Institute University Era of Space Access Access to space began 46 years ago (tomorrow) with the launch of Sputnik 1 aboard
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
The ROSETTA/CNSR Mission
The ROSETTA/CNSR Mission 88-009 A possible application of electric propulsion to interplanetary missions A. Atzei, 0/SCI, ESA/ESTEC, Noordwijk, The Netherlands 1. SUMMARY AND INTRODUCTION 4000 kg, including
Appendix B. A proposition for updating the environmental standards using real Earth Albedo and Earth IR Flux for Spacecraft Thermal Analysis
19 Appendix B A proposition for updating the environmental standards using real Earth Albedo and Earth IR Romain Peyrou-Lauga (ESA/ESTEC, The Netherlands) 31 st European Space Thermal Analysis Workshop
Venus many opportunities for small satellites & probes A new view of Earth s sister: Insights following seven years of observations with Venus Express
Venus many opportunities for small satellites & probes A new view of Earth s sister: Colin Wilson Oxford University Insights following seven years of observations with Venus Express Dmitriy Titov European
A Concept for a Joint NASA/ESA Mission for In Situ Explora9on of an Ice Giant Planet
IPPW-15 Boulder, 2018 #581 A Concept for a Joint NASA/ESA Mission for In Situ Explora9on of an Ice Giant Planet D.H. Atkinson (David.H.Atkinson@jpl.nasa.gov), O. Mousis, T.R. Spilker, A. Coustenis, M.
VENUS ORBITER AND ENTRY PROBE: AN ESA TECHNOLOGY REFERENCE STUDY
In Proceedings of the 8th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2004' ESTEC, Noordwijk, The Netherlands, November 2-4, 2004 VENUS ORBITER AND ENTRY PROBE: AN ESA
Astronomy. physics.wm.edu/~hancock/171/ A. Dayle Hancock. Small 239. Office hours: MTWR 10-11am. Page 1
Astronomy A. Dayle Hancock adhancock@wm.edu Small 239 Office hours: MTWR 10-11am Planetology I Terrestrial and Jovian planets Similarities/differences between planetary satellites Surface and atmosphere
Astrodynamics tools in the ESTEC Concurrent Design Facility. Robin Biesbroek CDF Technical Assistant ESA/ESTEC Noordwijk - NL
Astrodynamics tools in the ESTEC Concurrent Design Facility Robin Biesbroek CDF Technical Assistant ESA/ESTEC Noordwijk - NL CDF Astrodynamics CDF Presentation - 1 Introduction Concurrent Design Facility
MISSION 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
Cosmic Vision : The scientific priorities for astrophysics and fundamental physics
Cosmic Vision 2015-2025: The scientific priorities for astrophysics and fundamental physics Fabio Favata ESA, Astronomy & Fundamental Physics Mission Coordinator Grand themes 1. What are the conditions
2.12 Venus Express. Introduction. Mission overview. Scientific goals
2.12 Venus Express Venus Express was launched from Baikonur Cosmodrome on 9 November 2005. A Soyuz-Fregat rocket put the 1200 kg spacecraft almost perfectly on the ideal trajectory towards Earth s twin
Propulsion Technology Assessment: Science and Enabling Technologies to Explore the Interstellar Medium
Propulsion Technology Assessment: Science and Enabling Technologies to Explore the Interstellar Medium January 2015 Les Johnson / NASA MSFC / ED04 www.nasa.gov Mission Statement Interstellar Probe Mission:
Lunar Flashlight Project
ABSTRACT Recent observations of the Moon with the Moon Mineralogy Mapper (M3), Lunar Crater Observation and Sensing Satellite (LCROSS), the Lunar Reconnaissance Orbiter (LRO) and other evidence suggest
The Quest for Interstellar Exploration
The Quest for Interstellar Exploration Richard A. Wallace and Juan A. Ayon Jet Propulsion Labovatory/California Institute of Technology, Pasadena, California 91 109 818-354-2797, RichardA. Wallace@pl.nasa.gov;
IAC-04-Q.2.a.02 SYSTEM CONCEPTS AND ENABLING TECHNOLOGIES FOR AN ESA LOW-COST MISSION TO JUPITER/EUROPA
IAC-04-Q.2.a.02 SYSTEM CONCEPTS AND ENABLING TECHNOLOGIES FOR AN ESA LOW-COST MISSION TO JUPITER/EUROPA Patrice Renard, Charles Koeck, Steve Kemble EADS-Astrium, France & United-Kingdom patrice.renard@astrium.eads.net,
Facts Largest Moon of Saturn. Has an atmosphere containing mostly Nitrogen and methane. 1 gram on Earth would weigh 0.14g on Titan. Only know moon in
Titan Martin E Facts Largest Moon of Saturn. Has an atmosphere containing mostly Nitrogen and methane. 1 gram on Earth would weigh 0.14g on Titan. Only know moon in our solar system to have a dense atmosphere.
Sushil Atreya. Venus Chapman Conference Key Largo, 16 February
Sushil Atreya Venus Chapman Conference Key Largo, 16 February 2006 The Venus Exploration Analysis Group (VEXAG) was established by NASA in July 2005 to identify scientific priorities and strategy for exploration
ASEN 5050 SPACEFLIGHT DYNAMICS Interplanetary
ASEN 5050 SPACEFLIGHT DYNAMICS Interplanetary Prof. Jeffrey S. Parker University of Colorado Boulder Lecture 29: Interplanetary 1 HW 8 is out Due Wednesday, Nov 12. J2 effect Using VOPs Announcements Reading:
ROSETTA. 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
Theme 2: Outer Solar System Tracing the origin of the Solar System
Theme 2: Outer Solar System Tracing the origin of the Solar System Essential for our understanding of the formation and evolution of our own Solar System Exploration of the outer solar system has traditionally
VENUS EXPRESS. The First European Mission to Venus. Gerhard Schwehm and Hakan Svedhem ESA/ESTEC
VENUS EXPRESS The First European Mission to Venus Gerhard Schwehm and Hakan Svedhem ESA/ESTEC Why is ESA going to Venus? Venus is a fascinating planet and an attractive target for planetary sciences. 1960-1990:
IAC-04-Q.2.a.02 SYSTEM CONCEPTS AND ENABLING TECHNOLOGIES FOR AN ESA LOW-COST MISSION TO JUPITER/EUROPA
IAC-04-Q.2.a.02 SYSTEM CONCEPTS AND ENABLING TECHNOLOGIES FOR AN ESA LOW-COST MISSION TO JUPITER/EUROPA Patrice Renard, Charles Koeck, Steve Kemble EADS-Astrium, France & United-Kingdom patrice.renard@astrium.eads.net,
Recent Advances and Low cost concept for the Gamma-Ray Lens Project MAX
. Page 1 Recent Advances and Low cost concept for the Gamma-Ray Lens Project MAX ---- F. Arbusti a, P. Attina b X. Leyre a, M. Sghedoni a a Alcatel Alenia Space - Cannes - France. b Alcatel Alenia Space
ASTEX An In-Situ Exploration Mission to two Near-Earth-Asteroids
ASTEX An In-Situ Exploration Mission to two Near-Earth-Asteroids A. Nathues 1, H. Boehnhardt 1, A. W. Harris 2, W. Goetz 1,C. Gritzner 3, C. Jentsch 4, N. Schmitz 2, S. Schaeff 6, F. Weischede 5, A. Wiegand
NEW HORIZONS 2. New Horizons: A Journey to New Frontiers
NEW HORIZONS 2 New Horizons: A Journey to New Frontiers WHY NEW HORIZONS 2? PROVIDE BACKUP FOR THE HIGHEST PRIORITY NF OBJECTIVE OF THE DECADAL SURVEY. ENABLE THE FIRST EXPLORATION OF A LARGE (500 KM CLASS)
Comparative Planetology I: Our Solar System. Chapter Seven
Comparative Planetology I: Our Solar System Chapter Seven ASTR 111 003 Fall 2006 Lecture 07 Oct. 16, 2006 Introduction To Modern Astronomy I Introducing Astronomy (chap. 1-6) Planets and Moons (chap. 7-17)
MAE 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
ASPECT Spectral Imager CubeSat Mission to Didymos
ASPECT Spectral Imager CubeSat Mission to Didymos Kestilä A. 1),Näsilä A. 2), Kohout T. 3),Tikka T. 1),Granvik M. 3) 1. Aalto University, Finland. 2. Technical Research Center of Finland, Finland 3. Helsinki
DARE 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
European Venus Explorer
European Venus Explorer An in-situ Venus explorer proposed in Dec 2010 as a Cosmic Vision M3 mission, for launch in 2020 2025 Colin Wilson co - P.I. Univ. of Oxford & Eric Chassefière P.I. Univ. Paris
Lecture #27: Saturn. The Main Point. The Jovian Planets. Basic Properties of Saturn. Saturn:
Lecture #27: Saturn Saturn: General properties. Atmosphere. Interior. Origin and evolution. Reading: Chapters 7.1 (Saturn) and 11.1. The Main Point Saturn is a large Jovian-class planet with a composition
Juno Status and Earth Flyby Plans. C. J. Hansen
Juno Status and Earth Flyby Plans C. J. Hansen July 2013 Juno will improve our understanding of the history of the solar system by investigating the origin and evolution of Jupiter. To accomplish this