Gravity Gradient sensor technology for future planetary missions ESA ITT AO/1-3829/01/NL/ND Moons around Jupiter Io Europa ESTEC September 23 2005 University.

Slides:



Advertisements
Similar presentations
Atom Chip Technology (ACT) A New Program to Focus a New Quantum Technology for Emerging National Needs CQI Please See Nick Bigelow With Questions.
Advertisements

HgCdTe Avalanche Photodiode Arrays for Wavefront Sensing and Interferometry Applications Ian Baker* and Gert Finger** *SELEX Sensors and Airborne Systems.
Towards Low-cost Swedish Planetary Missions S. Barabash 1, O. Norberg 2, J.-E. Wahlund 3, M. Yamauchi 1, S. Grahn 4, S. Persson 4, and L. Blomberg 5 1.
September 23, 2004Univeristy of Twente1 Superconducting Gravity Gradiometry State of the Art.
Wafer Level Packaging: A Foundry Perspective
Analysis of Spark Ignition Engine Management System
The Sun Current Age (and predicted lifetime) Mass (kg and also Earth Masses) Size (radius in m and Earth radii) Surface Temperature (in Kelvin) Chemical.
Method of beam extraction from a synchrotron by the instrumentality of multilayer Cu-Fe shield Bondarenko Alexey.
Variable Capacitance Transducers The Capacitance of a two plate capacitor is given by A – Overlapping Area x – Gap width k – Dielectric constant Permitivity.
1 The Jovian Planets. 2 Topics l Introduction l Images l General Properties l General Structure l Jupiter l Summary.
Ryan Roberts Gyroscopes.
FluxDemon FluxDemonSat Fluxgate Magnetometer Core Technology Demonstrator Feasibility Review Student Design Team: Farita Tasnim, Shivani Upadhayay, Jinny.
April 27th, 2006 Paola Puppo – INFN Roma ILIAS Cryogenic payloads and cooling systems (towards a third generation interferometer) part II: the Vibration.
Measurements using Atom Free Fall
2/9/2006Welcome to LIGO1 Welcome to LIGO!. 2/9/2006Welcome to LIGO2 LIGO: A detector that measures very tiny displacements How tiny?
Paik-1 Inverse-Square Law Experiment in Space: Search for Extra Dimensions Ho Jung Paik, Violeta Prieto, M. Vol Moody University of Maryland and Donald.
GG 450 Magnetism February 7, QUIZ Like gravity, magnetic fields are POTENTIAL fields, and we expect that we will be able to trade vectors for scalars.
“Galileo Galilei” (GG) GG Phase A-2 Study funded by ASI ongoing at TAS-I (TO) with support from GG/GGG scientists GG target: test the Equivalence Principle.
Paik-1 Exploring Gravity with Proof-Mass Technologies Ho Jung Paik University of Maryland July 6-10, 2008, Warrenton, VA.
Lecture II Non dissipative traps Evaporative cooling Bose-Einstein condensation.
MEMS for NEMS Solutions for the Fat Finger Problem Michael Kraft.
A presentation by Jared Stachiw PhD, MPhil and Devon Burmeister P.Eng., BA.
Introduction to HYPER Measuring Lense-Thirring with Atom Interferometry P. BOUYER Laboratoire Charles Fabry de l’Institut d’Optique Orsay, France.
Solar System J. Wunderlich, Ph.D. Image from
Light Pulse Atom Interferometry for Precision Measurement
Gravity Section 1-2.
Paul C. Haljan University of Michigan Oct I. Laser cooling atoms Magnets Lasers.
G O D D A R D S P A C E F L I G H T C E N T E R 1 GW Interferometry at Goddard Space Flight Center Jordan Camp NASA / Goddard Space Flight Center Jan.
Österreichische Akademie der Wissenschaften (ÖAW) / Institut für Weltraumforschung (IWF), Graz, Austria, T +43/316/ , iwf.oeaw.ac.atDownload:2013.
Southwest Research Institute NSF Conference on Small Satellites Plasma Instrument Miniaturization and Integration: Approaches and Limitations C.J. Pollock,
Slide # 1 Velocity sensor Specifications for electromagnetic velocity sensor Velocity sensors can utilize the same principles of displacement sensor, and.
Computer Simulations in Solar System Physics Mats Holmström Swedish Institute of Space Physics (IRF) Forskarskolan i rymdteknik Göteborg 12 September 2005.
Brief introduction of YINGHUO-1 Micro-satellite for Mars environment exploration J. Wu, G. Zhu, H. Zhao, C. Wang, L. Lei, Y. Sun, W. Guo and S. Huang Center.
FluxDemon FluxDemonSat Fluxgate Magnetometer Core Technology Demonstrator Feasibility Review Student Design Team: Farita Tasnim, Shivani Upadhayay, Jinny.
Length: 203 cm Weight: 13.9 k.g Diameter: 15 cm Launch Vehicle: Juno |
Why do we put the micro in microelectronics?. Why Micro? 1.Lower Energy and Resources for Fabrication 2.Large Arrays 3.Minimally Invasive 4.Disposable.
Obtaining Ion and Electron Beams From a source of Laser-Cooled Atoms Alexa Parker, Gosforth Academy  Project Supervisor: Dr Kevin Weatherill Department.
PeTeR: a hardware simulator for LISA PF TM-GRS system 23/05/ th LISA Symposium May 2012, BnF Paris L. Marconi and R. Stanga Università degli.
Standard Form Recap – Planetary Data Sun mass kg.
Moon The Moon is the Earth’s only natural satellite and was formed 4.6 billion years ago around some million years after the formation of the solar.
The Potential Use of the LTMPF for Fundamental Physics Studies on the ISS Talso Chui Jet Propulsion Laboratory, California Institute of Technology, Pasadena,
The Sun The Sun is a star. The Sun is a star. It is 4,500 million years old It is 4,500 million years old It takes 8 minutes for its light to reach.
Law of Universal Gravitation Law of Universal Gravitation: gravity is a force of attraction that exists between any two objects that have mass. Force of.
The formation of the solar system.. The Planets in Our Solar System Planet Distance from the Sun (Astrono mical Units miles km) Period of Revolut ion.
Lunar Surface Atmosphere Spectrometer (LSAS) Objectives: The instrument LSAS is designed to study the composition and structure of the Lunar atmosphere.
G O D D A R D S P A C E F L I G H T C E N T E R 1 Status of LISA Jordan Camp LISA Deputy Project Scientist NASA / Goddard Space Flight Center Jan. 19,
1 Kazuhiro Yamamoto Institute for Cosmic Ray Research The university of Tokyo LCGT internal review (Cryogenic payload) 30 January 2012.
A WIRELESS PASSIVE SENSOR FOR TEMPERATURE COMPENSATED REMOTE PH MONITORING IEEE SENSORS JOURNAL VOLUME 13, NO.6, JUNE 2013 WEN-TSAI SUNG, YAO-CHI HSU Ching-Hong.
The Solar System The Moon The Earth The Sun How do they move? Why doesn’t the Earth fly away? Photos by NASA.
NMLTA Protection System Update -Loss Monitors- Arden Warner September 2 nd, 2009.
Aerospace technology 07 July 2016 Magnetómetros nos satélites da ESA e a aplicação dos MEMS no espaço Strictly Confidential.
Testing general relativity experimentally: Equivalence Principle Tests
Shape Memory Alloy Reusable Deployment Mechanism
Variable Capacitance Transducers
All About jupiter By: Logan.
Micro-channel Cooling
Quantum Technology gravity sensors – first steps to aerial sensing
Structure and etc Shoji Uno (KEK) at B2GM
Newtonian Physics – 10 Mr. Jean
Laser Harp MIDI Controller with Musical Articulations
Gravity field and steady-state Ocean Circulation Explorer
Inverse Square Sensitivity
Standard Form Recap –.
Kinetic Theory and a Model for Gases
What force?????.
Standard Form Recap –.
Kinetic Theory and a Model for Gases
How do objects move under the influence of gravity?
Cold Atom project 12/02/2019.
CHEOPS - CHaracterizing ExOPlanet Satellite
Presentation transcript:

Gravity Gradient sensor technology for future planetary missions ESA ITT AO/1-3829/01/NL/ND Moons around Jupiter Io Europa ESTEC September University of Twente University of Nantes R&D Programme

Programme for planetary exploration presented by Christophe Sotin

Programme for instrument development Gravity gradiometers based on MEMS and hybrid MEMS orbiter aerial vehicles/balloons (mapping smaller area) Laser cooled atom interferometry Multi sensor multi satellite systems formation flying

MEMS-based GG systems important parameters mass, base line, temperature, quality factor, operating frequency design of prototype with sensitivity in range mE/√Hz further development necessary

MEMS-based GG systems First generation devices: accelerometers and gradiometers with moderate sensitivity fabrication of several devices with different spring approaches material selection for electrodes charge trapping studies by C-V and C-t measurements (pull-in voltage, built-in voltage, temperature effects. electronic readout, force feedback, integration on MEMS-device Second generation devices: Improvement of first generation devices with respect to sensitivity Hybrid systems consisting of MEMS plus additional test mass Study of floating systems Study of modulation of spring constants Inductive readout and the use of high Tc devices

MicroNED activities Several programmes within MicroNed: 250 researchers: 9 knowledge institutes, 23 companies total budget M€ 28 (to be matched) Microsatellite programme MISAT - development of a new generation of microsatellites, with formation flying abilities - payload development: gravity gradiometers, cooling - possible tests of instruments in space UT -development of some prototypes (1 PhD student) -further support necessary: Post Doc, technician, clean room costs -further ESA support would be great

Atom interferometry Conclusions Measurement is performed with the atom cloud in free falling, hence absolute value of gravity determines size, measuring time In space small sizes and long measuring time are possible Rb atoms are favorable with respect to cold collisions frequency shift A sensor for gravity gradient based on atom interferometry could achieve a sensitivity below 1 mE/√Hz using 10s interrogation time. Sizes: 10 cm diameter vacuum chambers, base line 1m Mass: some kg

Source: M. Kasevich, CAMOS Prospects for atom interferometry Waveguides in atom chips

Multi sensor multi satellite systems Programme within Microned - distance sensing (flight configuration) - gravity sensing (accelerometers) large base line systems - magnetic sensing ( GMR, flux gates, high Tc devices) UT 1 PhD student Additional support from ESA?

National Platform planetary research Established on October 29 in 2004 Strengthen the relation between the Dutch potential for planetary research institutions, universities, industries Concentration Astrophysics Instruments (search for live, polarimeter, gravity gradiometers) Focussing on Mars