Dec 1, 2012 1 FIELDS Top Level Requirements Review S. Harris (UCB)

Slides:



Advertisements
Similar presentations
Paul T.M. Loto’aniu 1,2 and H.J. Singer 1 NOAA Space Environment Center 1 CIRES, University of Colorado 2 Paul T.M. Loto’aniu 1,2 and H.J. Singer 1 NOAA.
Advertisements

Solar Energetic Particle Production (SEPP) Mission Primary Contacts: Robert P. Lin (UC Berkeley), John L. Kohl (Harvard-Smithsonian CfA) Primary Science.
Classical vs Quantum Mechanics Rutherford’s model of the atom: electrons orbiting around a dense, massive positive nucleus Expected to be able to use classical.
The Frequency Agile Solar Radiotelescope Current Status & Plans T. S. Bastian NRAO.
Solar system science using X-Rays Magnetosheath dynamics Shock – shock interactions Auroral X-ray emissions Solar X-rays Comets Other planets Not discussed.
DOPPLER DOPPLER A Space Weather Doppler Imager Mission Concept Exploration Science Objectives What are the most relevant observational signatures of flare,
990901EIS_RR_Science.1 Science Investigation Goals and Instrument Requirements Dr. George A. Doschek EIS US Principal Investigator Naval Research Laboratory.
Solar Probe Plus FIELDS Monthly Management Telecom Sep 17, 2012.
Telecom 1 9/17/2012 SPP/FIELDS Solar Probe Plus FIELDS Monthly Management Telecom Sep 17, 2012.
Stuart D. BaleFIELDS iCDR – Science Requirements Solar Probe Plus FIELDS Instrument CDR Science and Instrument Overview Science Requirements Stuart D.
The FIELDS Instrument Suite Stuart D
Solar Probe Plus A NASA Mission to Touch the Sun Solar Probe Plus Science Workshop March 26, 2013 Solar Probe Plus A NASA Mission to Touch the Sun Nicky.
The Sun and the Heliosphere: some basic concepts…
Solar Probe Plus FIELDS Quarterly Management Nov 15, 2012.
Dale E. Gary Professor, Physics, Center for Solar-Terrestrial Research New Jersey Institute of Technology 1 03/15/2012Preliminary Design Review.
Electromagnetic Spectrum
SPP/FIELDS System Engineering Preliminary Design Review
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW CDR /30-10/1 27 EFW Science Overview Professor John R. Wygant (PI) University.
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.
Solar Probe Plus A NASA Mission to Touch the Sun Solar Probe Plus – A Mission to Touch the Sun Rob Decker and Nicky Fox Johns Hopkins Applied Physics Laboratory.
EFW Data Products/Processing Van Allen Probe SWG San Antonio September 2104 J.R. Wygant, J. Bonnell, Aaron Breneman, S. Thaller and the EFW Team.
Solar System Missions Division Solar Orbiter Next major Solar and Heliospheric mission ESA ILWS flagship Now with the Inner Heliospheric Sentinels.
China National Report , Prague, Czech Republic.
Remote Radio Sounding Science For JIMO J. L. Green, B. W. Reinisch, P. Song, S. F. Fung, R. F. Benson, W. W. L. Taylor, J. F. Cooper, L. Garcia, D. Gallagher,
Stuart D. BaleFIELDS iPDR – Science Requirements Solar Probe Plus FIELDS Instrument PDR Science and Instrument Overview Science Requirements Stuart D.
GoetzFIELDS Quarterly – 18 July 2013 SPP/FIELDS Modes and Operations Stuart D. Bale, Keith Goetz 18 July
195 Å image – behind 195 Å image – Sun- Earth line – SOHO/ EIT image 195 Å image – Sun- Earth line – SOHO/ EIT image 195 Å image – ahead SECCHI Extreme.
THEMIS MISSION PDROVERVIEW- 1 UCB, November 12, UCB/Swales should identify an individual that will assume responsibility for magnetic cleanliness.
Graz, June 2007 The DEMETER mission: Objectives and first results M. Parrot LPCE/CNRS 3A, Avenue de la Recherche Orléans cedex 2, France
China National Report , Uppsala, Sweden China National Space Administration.
STAMMS Conference Meeting, Orleans, France May 2003 R. L. Mutel, D. A. Gurnett, I. Christopher, M. Schlax University of Iowa Spatial and Temporal Properties.
Large-Amplitude Electric Fields Associated with Bursty Bulk Flow Braking in the Earth’s Plasma Sheet R. E. Ergun et al., JGR (2014) Speaker: Zhao Duo.
The Solar Orbiter mission Solar Orbiter represents a new approach to solar studies. –A huge increase in discovery space The payload consists of a suite.
1 Mars Micro-satellite Mission Japanese micro-satellite mission to Mars to study the plasma environment and the solar wind interaction with a weakly-magnetized.
STEREO: Beyond 3D. Why the Sun? The sun provides energy for the development of life on our planet. Our orbit looks calm and peaceful, but there is nothing.
The investigations of the solar wind with the large decametric radio telescopes of Ukraine Falkovych I.S. 1, Konovalenko A.A 1, Kalinichenko N.N. 1, Olyak.
Observatoire de Paris University of Minnesota University of California - Berkeley Goddard Space Flight Center STEREO SWG, Fall Hills, Meredith, NH STEREO/WAVES.
Исследование широкополосной ELF турбулентности по данным спутника FAST И.В. Головчанская, Б.В. Козелов, И.В. Дэспирак Полярный геофизический институт.
Boston University Daniel TaylorNima Badizadegan R. Terry BlackPantelis Thomadis.
1 MAVEN PFP ICDR May 23-25, 2011 Mars Atmosphere and Volatile EvolutioN (MAVEN) Mission Particles and Fields Science Critical Design Review May ,
7 3-4 Sept EFW INST+SOC PDR EFW Science Overview Professor John R. Wygant (PI) University of Minnesota.
Space Research Institute Russian magnetospheric & heliospheric missions.
Space Research Institute BMSW - Fast Monitor of Solar Wind Plasma Parameters for current and future missions. M. Riazantseva 1,2, G. Zastenker 1, J. Safrankova.
CALIBRATION OF THE STEREO ANTENNAS AT LOW FREQUENCIES To measure Electric Fields To measure density fluctuations especially in the ion cyclotron frequency.
Jun 4, SPP FIELDS Updated block diagrams Fault Tolerant Design.
SWGTemplate- 1 UCB, Nov 15/16, 2006 THEMIS SCIENCE WORKING TEAM MEETING Search Coil Magnetometer (SCM) team Co-i: A. Roux, O. Le Contel Technical Manager(*):
Intermittency Analysis and Spatial Dependence of Magnetic Field Disturbances in the Fast Solar Wind Sunny W. Y. Tam 1 and Ya-Hui Yang 2 1 Institute of.
NASA NAG Structure and Dynamics of the Near Earth Large-Scale Electric Field During Major Geomagnetic Storms P-I John R. Wygant Assoc. Professor.
EFW SOC DATA John Wygant SWG June Redondo Beach.
How ARTEMIS Contributes to Key NLSI Objectives C.T. Russell, J. Halekas, V. Angelopoulos, et al. NLSI Lunar Science Conference Ames Research Center Monday,
Electric field, electric potential, and ‘density’ measurements at quasi-perpendicular collisionless shocks: Cluster/EFW measurements Stuart D. Bale, Ryan.
Stuart D. BaleFIELDS SOC CDR – Science Requirements Solar Probe Plus FIELDS SOC CDR Science and Instrument Overview Science Requirements Stuart D. Bale.
Solar observations with single LOFAR stations C. Vocks 1. Introduction: Solar Radio radiation 2. Observations with single LOFAR stations 3. Spectrometer.
Welcome to Uppsala! Thursday May 18 13:00, room Å :00 Coffee (17:30 Dinner) Friday May 19 09:00, room Å :00 Coffee splinters (other locations)
IDPU F1 Test Review FGM Fluxgate Magnetometer Michael Ludlam University of California - Berkeley.
Double Star Active Archive - DWP/STAFF 1 Double Star Active Archive STAFF/DWP Keith Yearby and Hugo Alleyne University of Sheffield Nicole Cornilleau-Wehrlin.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW I-PER 21 January EFW Science Overview Professor John R. Wygant, PI University.
Solar Probe Plus Payload Requirements Document Peer Review
Solar Probe Plus – FIELDS Main Electronics Package
Solar and heliosheric WG
Chengming Tan National Astronomical Observatories
Solar Probe Plus FIELDS MEP iPSR SOC Marc Pulupa April 10, 2017
INSTRUMENT DATA PROCESSING UNIT (IDPU) REQUIREMENTS
SWAVES-like radio instrument?
ARTEMIS – solar wind/ shocks
Solar Probe Plus – SWG September 2, 2016
SP+ DFB REE 12/01/12.
Solar Probe Plus FIELDS Instrument PSR - MEP Introduction
NASA NASA's Parker Solar Probe mission set off to explore the Sun's atmosphere on Sunday morning August 12, It will swoop to within 4 million miles.
Transition Region and Coronal Explorer (TRACE)
Presentation transcript:

Dec 1, FIELDS Top Level Requirements Review S. Harris (UCB)

Dec 1, 2012 Level 1 Requirements for SPP (for FIELDS) FIELDS Investigation description This investigation will make direct measurements of electric and magnetic fields and waves, Poynting flux, absolute plasma density and electron temperature, spacecraft floating potential and density fluctuations, and radio emissions. For Baseline Science, SPP will: –Measure magnetic and electric fields, their fluctuations and variations with sufficient cadence and sensitivity to identify and characterize solar wind structures (shocks, current sheets, discontinuities, and CMEs) –Analyze fluctuations and turbulence down to the dissipation range –Identify and quantify energy flux in the waves thought responsible for coronal and solar wind heating –Measure interplanetary radio emission with sufficient sensitivity and time resolution to resolve signatures of microflare coronal heating –Baseline measurements, shall be made at least between 9.5 Rs and 55 Rs: 2

Dec 1, 2012 Level 1 Requirements, continued For Threshold Science (minimum design requirements) –Threshold shall be met by making reduced capability measurements during first solar pass reaching 9.5 Rs and at least 500 hours within 20 Rs –Required threshold measurements: 3

Dec 1, 2012 Level 2 Requirements for SPP FIELDS-Centric L2 Requirements… Make measurements as described in L1 Baseline Complete at least three orbits with Perihelion < 10 Rs S/C must Accommodate: –4 electric field antennas –2 fluxgate magnetometers –One 3-axis search coil magnetometer S/C is required to provide thruster indicator to instruments Absolute time knowledge accuracy for FIELDS is ±1 sec (3  ) –After post processing on the ground S/C is required to reorient S/C to support calibration and provide real time telemetry during commissioning S/C pointing control, alignment, knowledge (for FIELDS) is 3° – Other instruments are tighter, WISPR requires 1° pointing – Mission req’t is pointing knowledge wrt Sun center: better than 1° (3  ) S/C required to dowlink avg of 85 Gbits science data / orbit – FIELDS allocation is currently 20Gbits/orbit, avg rate of 26kbps 4

Dec 1, 2012 Level 3 Payload Requirements - MAG MAG Requirements… –Bandwidth required is lower than planned MAG performance –Two ranges specified: 65536nT and 4096nT –Sensitivity is consistent with GSFC MAG performance –Accuracy specified to 5nT –3D vectors specified –Solar distances 9.5 Rs to 0.25AU (shows up on all requirements) 5 Requirement Rationale

Dec 1, 2012 Level 3 Payload Requirements - SCM SCM requirements… –Performance based on a FIELDS presentation of 8/10/2012 “FIELDS_EMC_summary_ pdf” Stuart Bale –Accuracy specified to 1dB –3D vectors specified 6 Requirement Rationale

Dec 1, 2012 Level 3 Payload Requirements – DFB Survey Measurement requirements for DFB Survey… –SCM not included –32 samples/s –Two orthogonal directions 7 The Plasma Wave Investigation shall provide electric fields measurements for MHD Scale Physics (DFB Survey Mode) for solar orbital distances of 9.5 Rs to 0.25 AU, as follows: -- cadence of 32 samples/s (Nyquist frequency of 16 Hz) [TBR]; -- magnitude range: 0 to 500 mV/m [TBR]; -- sensitivity of 1 mV/m [TBR]; -- in two orthogonal directions Requirement

Dec 1, 2012 Level 3 Payload Req. – DFB Burst Mode 1 Measurement requirements for DFB Burst Mode 1… –SCM not included –256 samples/s –Dynamic range: 140dB (7 decades) –Sensitivity: 100 µV/m / √Hz at 75Hz –Two orthogonal directions 8 The Plasma Wave Investigation shall provide electric fields measurements for Ion Scale Physics (DFB Burst Mode 1) for solar orbital distances of 9.5 Rs to 0.25 AU, as follows: -- cadence of 256 samples/s (Nyquist frequency of 128 Hz)[TBR]; -- dynamic range of 140 dB [TBR]; -- sensitivity of 1 x 10^(-4) V/m/√Hz at 75 Hz [TBR] -- in two orthogonal directions Requirement

Dec 1, 2012 Level 3 Payload Req. – DFB Burst Mode 2 Measurement requirements for DFB Burst Mode 2… –SCM not included –128k samples/s –Dynamic range: 140dB (7 decades) –Sensitivity: 1 µV/m / √Hz at 3.5kHz –Two orthogonal directions 9 The Plasma Wave Investigation shall provide electric fields measurements for Electron Scale Physics (DFB Burst Mode 2), for solar orbital distance of 9.5 Rs to 0.25 AU, as follows: -- cadence of 128k samples/s (Nyquist frequency of 64 KHz) [TBR]; -- dynamic range of 140 dB [TBR]; -- sensitivity of 1 x 10^(-6) V/m/√Hz at 3.5 kHz [TBR] -- in two orthogonal directions Requirement

Dec 1, 2012 Level 3 Payload Req. – TDS Burst Mode Measurement requirements for TDS Burst Mode… –SCM not included –2M samples/s –Dynamic range: 140dB (7 decades) –Sensitivity: 0.1 µV/m / √Hz at 100kHz –Two orthogonal directions 10 The Plasma Wave Investigation shall provide electric fields measurements for Microphysics (TDS Burst Mode) for solar orbital distances of 9.5 Rs to 0.25 AU, as follows: -- cadence of 2 M samples/sec (Nyquist frequency of 1 M Hz) [TBR]; -- dynamic range of 140 dB [TBR]; -- sensitivity of 1 x 10^(-7) V/m/√Hz at 100 kHz [TBR] -- in two orthogonal directions Requirement

Dec 1, 2012 Level 3 Payload Req. – DFB Spectral Mode Measurement requirements for DFB Spectra… –1 spectra/s, 1Hz to 64kHz (in variance with DFB expectation?) –Dynamic range: 140dB –Two orthogonal directions –No specification for resolution 11 The Plasma Wave Investigation shall provide electric fields measurements for Turbulence/Wave Spectra (DFB Spectral Mode) for solar orbital distances of 9.5 Rs to 0.25 AU, as follows: -- cadence of 1 spectrum/sec [TBR]; -- frequency range of 1Hz to 64 kHz; -- dynamic range of 140 dB [TBR]; -- sensitivity of (1) 1 x10^(-4) V/m/√Hz at 75 Hz [TBR]; (2) 1 x10^(-6) V/m/√Hz at 3.5 KHz [TBR]; -- in two orthogonal directions Requirement

Dec 1, 2012 Level 3 Payload Req. – QTN Spectroscopy Measurement requirements for QTN Spectra… –1 spectra/4s, 10Hz to 2.5MHz –Dynamic range: 100dB –Two orthogonal directions –No specification for resolution 12 The Plasma Wave Investigation shall provide electric fields measurements for QTN Spectroscopy (TNR/HFR Survey Mode) for solar orbital distances of 9.5 Rs to 0.25 AU, as follows: -- cadence of 1 spectrum / 4 sec [TBR]; -- frequency range of 10 kHz to 2.50 MHz; -- dynamic range of 100 dB [TBR]; -- sensitivity of 2 x 10^(-7) V/m/√Hz at 1 MHz [TBR]; -- in two orthogonal directions Requirement

Dec 1, 2012 Level 3 Payload Req. – Radio Emissions Measurement requirements for Radio Frequency Spectra… –1 spectra/16s, 1MHz to 16MHz (in variance with DFB expectation?) –Dynamic range: 80dB –Two orthogonal directions –No specification for resolution 13 The Plasma Wave Investigation shall provide electric fields measurements for Radio Emissions (TNR/HFR Survey Mode) for solar orbital distances of 9.5 Rs to 0.25 AU, as follows: -- cadence of 1 spectrum / 16 sec [TBR]; -- frequency range of 1 MHz to 16 MHz; -- dynamic range of 80 dB [TBR]; -- sensitivity of 1 x 10^(-7) V/m/√Hz at 10 MHz [TBR]; -- in two orthogonal directions Requirement

Dec 1, 2012 Other Level 3 Payload Req. – Some highlights Provide at least 3 orbits of science measurements reaching perihelion distance of 9.5 Rs Provide at least 950 hours of measurements below 20 Rs Operational lifetime of 7 years after launch Accommodate in-flight calibration FIELDS shall participate in system-wide burst mode –Share limited amount on instrument messaging for coordinating burst –Share status packets at 1Hz that includes status and burst data Receive/react to S/C time/status packet –Includes burst flags, shared burst data, MET, S/C status indicators –e.g. thruster status, SSR status, distance from sun, power down req. FIELDS shall provide for exchange of data with SWEAP Limit internal timing uncertainty to ±1ms Limit total internal alignment error < 1 ° (dynamic + static) FIELDS shall implement time-tagged command functionality, if req’d. Antennas shall provide features to compensate for TPS shifts Survive and/or meet L3 performance during Solar Storm events 14