PHILAE Science Team, Venice 20091 Philae On-Comet Science Objectives prepared by HBO Document name = Scientific Objectives of the PHILAE Mission (RO-LAN-LI-1000),

Slides:



Advertisements
Similar presentations
M.A.D.A.N.A.C Ph. Bendjoya L.U.A.N-U.N.S/C.N.R.S A. Cellino Osservatorio di Torino I.N.A.F M.A.D.A.N.A.C Measurement And Discovery of Asteroids and NEOs.
Advertisements

The BepiColombo Mission
Solar System Division DVK, 10 Jul 2001 Rosetta Science Operations The planning concept - current status Detlef Koschny Space Science Department ESA/ESTEC.
Philae Science Team Meeting Venice, 30 Mar. – 1 Apr Rita Schulz - Rosetta - Mission Status.
Payload Site One Upon landing, the LOW prepares for single-site goals and multi-site goals. A drop-box is prepared for single-site goals utilizing various.
Deep Impact Projectsmfa - 1 Deep Impact Projects (2) Mike A’Hearn.
Mission: Launch 2014/15; Deployment June-August 2019, release alt. 100m Mission duration: 16 hrs of on-asteroid operation Main functions: On-surface up-righting.
Minor bodies observation from Earth and space: asteroid (2867)Steins A. Coradini, M.T. Capria, F. Capaccioni, and the VIRTIS International Team.
OIB Long Range Planning Luthcke and Jezek. OIB Long Term Observation Goals OIB is meant to provide data to improve our understanding of the mass evolution.
Philae Science team meeting. Venezia, March 30, 31, April 1, 2009Palazzo Cavalli Franchetti.
4th Philae Science Workshop, Venice th Philae Science Workshop Venice, 30 March – 1 April ROMAP Status I. Apáthy, U. Auster, G. Berghofer, A.P.
Solar Energetic Particle Production (SEPP) Mission Primary Contacts: Robert P. Lin (UC Berkeley), John L. Kohl (Harvard-Smithsonian CfA) Primary Science.
Philae Science team meeting Venezia, March 30, 31, April 1, 2009 Palazzo Cavalli Franchetti 1. Instrument status Final discussion and wrap-up.
Open Cruise Requirements status and planning LSWT#4, Venice 30/03-01/ LSWT#4.
Physics 681: Solar Physics and Instrumentation – Lecture 4
PHILAE Science Team, Venice LTS phase: the LS standpoint prepared by HBO LTS phase: from end of FSS (mid Nov. 2014) to end of Rosetta mission (31.
PLASMA DISCHARGE SIMULATIONS IN WATER WITH PRE-EXISTING BUBBLES AND ELECTRIC FIELD RAREFACTION Wei Tian and Mark J. Kushner University of Michigan, Ann.
Philae Status and News Venezia; 30 st of March th Philae Post-Launch Workshop.
SDL: MOST point of view CNES / J-F Fronton / D Hallouard LSWT Venice, 30/03-01/04/2009.
The flight dynamics standpoint Alejandro Blazquez (CNES)‏ LSWT Venice, 30/03-01/04/2009.
1 TEC-MTT/2012/3788/In/SL LMD1D v1 and v2 Comparison with Phoenix Flight Data Prepared by Stéphane Lapensée ESA-ESTEC, TEC-MTT Keplerlaan 1, 2201 AZ Noordwijk.
ISSI Meeting, Berne, Switzerland January, 2014 page 1 The scientific objectives of ESA’s Comet Orbiter ROSETTA and Lander PHILAE Susan McKenna-Lawlor.
1 Robert Schaefer and Joe Comberiate for the SSUSI Team Robert SchaeferJoe Comberiate (240) (240)
THE DIURNAL TEMPERATURE REGIME OF THE SURFICIAL REGOLITH OF PHOBOS IN THE LANDING SITE REGION OF THE FOBOS-GRUNT LANDER FOR DIFFERENT SEASONS: THE MODEL.
Measurement in Physical and Behavioral Sciences. The Nature of Measurement Measurement is a process of assigning numerals to observations according to.
Exploring Our Past, Securing Our Future Space Grant Symposium April 12 th 2014 Model-based Systems Engineering of The OSIRIS-REx Mission's Science Processing.
Folie 1 MUPUS Team Meeting, Graz> I. Pelivan> Thermal Model > Comet Engineering Thermal Model I. Pelivan, E. Kührt.
Pretest 1. True or False: Compounds have fixed compositions TRUE!
Molecular mass spectrometry Chapter 20 The study of “molecular ions” M + e -  M e -
EddiCam: The Eddington Photometric Camera EddiCam Definition Phase Kick-Off Meeting J. Miguel Mas-Hesse Vienna, 17th Sept., 2001.
Heliospheric Imager – Scientific Operations  HI Operations Document – R. Harrison  HI Image Simulation – C. Davis & R. Harrison  HI Operations Scenarios.
NETwork studies of MARS climate and interior A.V.Rodin, V.M.Linkin, A.N.Lipatov, V.N.Zharkov, T.V.Gudkova, R.O.Kuzmin.
Heliospheric Imager – Scientific Operations  HI Operations Document – R. Harrison (presented by Dave Neudegg – SciOps for Cluster, Mars Express, Double.
HEAT BLANKETING ENVELOPES OF NEUTRON STARS D.G. Yakovlev Ioffe Physical Technical Institute, St.-Petersburg, Russia Ladek Zdroj, February 2008, Outer crust.
Mars Geochemistry and Future Experiment Needs Mark A. Bullock August 7, 2002.
Bone Trajectories and Model Simulations Kathleen Mandt, Ray Goldstein, Christoph Koenders May 29, 2013 IES Team Meeting – San Antonio.
 Meteoroid – a chunk of rock or dust in space. (these come from comets or asteroids)  Meteor – a chunk of rock or dust that enters our atomosphere and.
Rosetta is the first mission designed to both orbit and land on a comet. It will complete.
Evaluating New Candidate Landing Sites on Mars: Current orbital assets have set the new standard for data required for identifying and qualifying new Mars.
Page 1 Validation Workshop, 9-13 th December 2002, ESRIN ENVISAT Validation Workshop AATSR Report Marianne Edwards Space Research Centre Department of.
1 MAVEN PFP ICDR May 23-25, 2011 Mars Atmosphere and Volatile EvolutioN (MAVEN) Mission Particles and Fields Science Critical Design Review May ,
CIVA Status Venezia, Palazzo Cavalli Franchetti March 31, 2009 Philae Science Team Meeting.
Физика плазмы в солнечной системе – 10-я конференция, ИКИ РАН, Эксперимент ФИЛА-РОМАР – плазменные измерения на поверхности кометы 67Р/ Чурумов-Герасименко.
Dean C. Hines Space Telescope Science Institute Precision Imaging Polarimetry with ACS.
DEEP IMPACT Mission To Comet 9P/Tempel 1. Deep Impact What Kind of Mission is it? A Discovery Mission Explore the interior of the nucleus of Comet 9P/Tempel.
Lunar Surface Atmosphere Spectrometer (LSAS) Objectives: The instrument LSAS is designed to study the composition and structure of the Lunar atmosphere.
Chapter 9 Stellar Atmospheres. Specific Intensity, I I ( or I ) is a vector (units: W m -2 Hz -1 sterad -1 )
G5/4 Revision Project Progress Update Andrew Bower
WG 2/3 Splinter meeting Dec. 6, 2010 ESOC Darmstadt for WG2 & WG3: D. Bockelée-Morvan C. Engrand E. Grün H. Krueger.
Workshop proposal to the Science Committee Solar Wind – Comet Surface Interaction.
Expected dust flux on OSIRIS J. Knollenberg
Rosetta Science Working Team Meeting #26 Working Group #1
RSOC Overview at SWT #26, 11/12 June 2009
ROSETTA SWT 27th ESOC, 2-4 December 2009
Pre-landing Orbiter Observations
OSIRIS Science planning
LET Performance Requirements Presenter: Richard Mewaldt
OSIRIS Full Team Meeting
Project Controls: As-Built S-Curves
SESAME: Surface Electric Sounding and Acoustic Monitoring Experiment
Philae status 21st Rosetta Science Team meeting
ROSINA, COSAC & PTOLEMY Reviewer: Heather Franz 2/15/16 – 2/17/16
Taking a Look at a Trojan Asteroid
SD2 Kevin Walsh 16 Feb, 2016.
Kinetic Theory.
→ASTEROID IMPACT MISSION
VIS/NIR sub-group discussion
Introduction- Link with WG E activity CMEP PLENARY MEETING-PRAGUE
ISO View Stereo Imaging Belly Cam GN&C
4. Complex Knowledge: demonstrations of learning that go aboveand above and beyond what was explicitly taught. 3. Knowledge: meeting the learning goals.
Presentation transcript:

PHILAE Science Team, Venice Philae On-Comet Science Objectives prepared by HBO Document name = Scientific Objectives of the PHILAE Mission (RO-LAN-LI-1000), tasks, 100 pages Document contains the experimenter’s objectives & wish list  it might not be possible to implement (operations) and to accomplish (experiments) all tasks Doc issue 1.0 released to ESA & PHILAE team by late Aug  lander objectives are considered in ESA’s planning of the ROSETTA science phase as a whole ESA has started science planning exercise through WGs science scenario approach

PHILAE Science Team, Venice Philae On-Comet Science Objectives prepared by HBO Issue 1.0 is incomplete and needs improvement for version some experiments have provided incomplete information of which only some details are indeed not known at the moment - most missing information: task priority, scenario descriptions, repetition cycles - experimenters focused on their respective instrument objectives - scenario approach with parallel/complementary measurements by other instruments (both onboard the lander and the orbiter) - for revision 2 new entry fields to be filled in - Expected Direct Measurement Result: The physical quantities that are obtained as immediate outcome of the experiment (without involving physical models). Usage of experiment models for characterizing the instrument are allowed. The expected physical units of the results should be listed as well. - Expected Results Through Modeling: The physical quantities that are obtained as indirect outcome of the experiment, now using physical models. Please identify the physical model or at least the type of physical model to be used and provide physical units of the results.

PHILAE Science Team, Venice Philae On-Comet Science Objectives prepared by HBO Return upon call for input for the revised document version 1.1 was insufficient positive: SD2, MUPUS, ROMAP, SESAME, COSAC, ROLIS nothing: APXS, CIVA, CONSERT, PTOLEMY Proposal on how to proceed towards a rather complete document with science priorities that are useful for planning purposes  PI teams: provide input as complete as possible  Easter 2009  LS compile version 1.1 and distribute it to PI teams  1 week thereafter  meeting of PIs and LSes with the task each PI: presentation of the respective science objectives all: discussion of science issues and pros & cons PIs: ranking of tasks per phase result: priority according to averaged ranking result

PHILAE Science Team, Venice 20094

5 Rosetta WG3 prepared by HBO Gas environment at cometary surface and along orbital path: capabilities: gas production, gas flux, gas density for chemical species accuracy (min,mean,max): 20/50/100% of actual regime at the surface resolution: spatial 0.5m at the surface, 10min timewise; typically every 0.01AU from the Sun along the orbit purpose: instrument and mission planning Dust environment at cometary surface and along orbital path: capabilities: dust production, dust flux, dust spatial density, dust size distribution, dust speed accuracy (min,mean,max): 20/50/100% of actual regime at the surface resolution: spatial 0.5m at the surface, 10min timewise; typically every 0.01AU from the Sun along the orbit purpose: instrument and mission planning

PHILAE Science Team, Venice Thermal environment at cometary surface and along orbital path: capabilities: nucleus temperature at different depth (0-40cm, each 5cm) accuracy (min,mean,max): 5/10/20C resolution: spatial 0.5m at the surface, 10min timewise; typically every 0.01AU from the Sun along the orbit purpose: instrument and mission planning Plasma and magnetic environment at cometary surface and along orbital path: capabilities: for ions and electrons plasma density, plasma flux, plasma temperature, ion composition; magnetic field strength and orientation accuracy (min,mean,max): 20/50/100 of actual regime at the surface resolution: spatial 0.5m at the surface, 10min timewise; typically every 0.01AU from the Sun along the orbit purpose: instrument and mission planning Rosetta WG3 prepared by HBO

PHILAE Science Team, Venice Light scattering environment at cometary surface and along orbital path: capabilities: 3D surface model with albedo and light scattering properties, dust production, dust size distribution, dust light scattering accuracy (min,mean,max): 20/50/100 of actual regime at the surface resolution: spatial 0.5m at the surface, 10min timewise; typically every 0.01AU from the Sun along the orbit purpose: instrument and mission planning Dust, gas and temperature environment at cometary surface and along orbital path: capabilities: dust density, dust flux, local gravity field, gas density, gas flux, gas composition, gas temperature, surface temperature of cometary environment at landing site accuracy (min,mean,max): 20/50/100 of actual regime at the surface resolution: spatial 0.5m at the surface, 10min timewise; typically every 0.01AU from the Sun along the orbit purpose: hazard avoidance Rosetta WG3 prepared by HBO

PHILAE Science Team, Venice Do we have models to contribute? Rosetta WG3 prepared by HBO