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THEMIS Introduction Nov 6, 2007.

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Presentation on theme: "THEMIS Introduction Nov 6, 2007."— Presentation transcript:

1 THEMIS Introduction Nov 6, 2007

2 Agenda Agenda Organization Schedule Mission Implementation
Mission Objectives Organization Schedule Mission Implementation S/C & Instrument Description Ground Systems Mission Operations

3 Substorms

4 Earth and Space Platforms
Aurora Current disruption Reconnection

5 Organization Program Organization PI Mode Cost and Schedule Caps
PI Team Provides Space, Ground, Data Segments PI Team Provides Cost, Schedule, Performance Assurance PI Team Provides Education/Public Outreach Cost and Schedule Caps Single Cost Cap for the Mission $180M (FY07) Launch no later than March 2007 (Launch Feb 2007) Performance Assurance MIDEX Quality Requirements Implementation Strategy Use Heritage Instrumentation Coordinate Common Buy Parts Keep Probe/Probe Carrier Simple and Robust Leave Complexity on the Ground Build & Verify Probe 1, then Probes 2-5

6 Mechanical/ Thermal Systems
Organization Mission Manager Frank Snow, GSFC Financial Mgr K. Harps, UCB Launch Vehicle G. Skrobott, KSC Project Scientist D. Sibeck, GSFC THEMIS PI V. Angelopoulos, UCB Project Manager P. Harvey, UCB Science Co-I’s EPO N. Craig, UCB Subcontracts J. Keenan, UCB Scheduling D. Meilhan, UCB Quality Assurance R. Jackson, UCB Mission Systems E. Taylor, UCB Mechanical/ Thermal Systems P. Turin, UCB C. Smith, UCB Mag Cleanliness C. Russell, UCLA Probe/Probe Carrier Management UCB Oversight: D. King Swales Mgr: M. Cully Instruments P. Berg, UCB Operations M. Bester, UCB Software Systems D. King, UCB Mission I&T J. McCauley, UCB R. Sterling, UCB

7 Organization Instruments P. Berg Electric Field Instrument (EFI)
J. Bonnell Electrostatic Analyzer (ESA) C. Carlson Solid State Telescope (SST) D. Larson Data Processor Unit (IDPU) M. Ludlam Fluxgate Mag (FGM) U. Auster Search Coil (SCM) A. Roux Forrest Mozer Greg Delory Art Hull Bill Donakowski Greg Dalton Robert Duck Dan Schickele Stu Harris Hilary Richard Robert Abiad Peter Berg Heath Bersch Dorothy Gordon Selda Heavner Jim Lewis Jeanine Potts Nestor Castillo C. Scholz M. Marckwardt Bill Elliott Ron Canario Robert Lee T. Moreau Hari Dharan Tien Tan Bill Tyler TUBS/IWF Uli Auster K. Glassmeier W. Magnes CETP Alain Roux Bertran de la Porte Olivier Le Contel Christophe Coillot A. Bouabdellah LASP Robert Ergun Aref Nammari Ken Stevens Jim Westfall Booms

8 Organization Ground Segment Mission Ops Science Ops Flight Dynamics
Ground Based Observatories Manfred Bester Mark Lewis Tim Quinn Sabine Frey Tai Phan All Sky Imagers Ground Magnetometers Fielding & Operation (UC&UA) Stephen Mende Stu Harris Harald Frey UCLA Chris Russell Joe Means Dave Pierce Bob Snare UC Eric Donovan GSFC/GCND David Sibeck Mark Beckman Bob DeFazio Rick Harman UA J. Samson

9 Mission Overview Launch Space Segment Ground Segment Operations
Vehicle: Delta II, Eastern Range Apogee: km ± 9567 km Perigee: 435 km ± 10 km (500 km ± 7 km on or after 3/1/2007) Inclination: 16.0 deg ± 0.5 deg Date: February 17, 2007 Space Segment Spacecraft: 5 Spinning Probes with Fuel for Orbit & Attitude Adjust Instruments: 3-Axis Electric Field, Magnetic Field 3-D Ion & Electron Particle Detectors Spin Rate: 20 RPM Orbit Period(s): 1, 2 and 4 days Orientation: Ecliptic Normal Ground Segment Observatories: 20 Northern with All Sky Imagers and Magnetometers Control Facilities: Mission and Science Operations Centers Operations Phases: L&EO, Cruise, Ascent, Campaigns, De-orbit Lifetime: 2.5 years

10 Instrument Configuration
IDPU: Instrument Data Processor Unit SPB : Spin Plane Booms (4x) AXB : Axial Booms (2x) SST : Solid State Telescope (2x) ESA : Electrostatic Analyzer FGM : Fluxgate Magnetometer SCM : Search Coil Magnetometer

11 Probe Configuration Antenna EFI Axial Booms (2, Stowed) ESA
Miniature Sun Sensor Fuel Tank IDPU EFI SPB Repress Tank Fuel Tank Transponder Thruster A2 Thruster T1 EFI SPB Thruster A1 BAU Battery Gyros EFI SPB Thruster T2 AEB 11

12 Launch Vehicle

13 Mission Data Flows THEMIS Probe TDRS Berkeley Ground Station Wallops Ground Station KSC & Astrotech (1) (3) Merritt Island Ground Station UCB I&T Facility JPL I&T Facility Compatibility Test Van White Sands Complex (3) (3) Secure Intranet Santiago Ground Station Secure VPN Tunnel via Open Internet (2) GSFC NMC Open IONet Dial-up ISDN Line Berkeley Mission Operations Center Notes: Open (1), Restricted (2) or Closed (3) IONet Hartebeesthoek Ground Station Different Routes for End-to-end Data Flows Between Probes and GS Elements

14 Ground Based Observatories
UCB/UCLA Delivered All 20 GBO (GMAG and ASI) units Automatic Data Collection and Archiving in Progress Remote Commanding and Diagnostics Working Courtesy H.Frey, UCB Geographic Longitude 324° Longitude 195° Geomagnetic North Pole

15 Ground Based Observatories
GBO Sites EPO Sites

16 Ground Based Data Flows

17 Schedule

18 Major Reviews

19 Probe 2 I&T F2 I&T at UCB Magnetics at JPL EMC at JPL VIB at JPL
TV at JPL Probe Fit Check

20 FM2/FM3 Thermal Vacuum Probes 1,3,4,5 I&T FM4/5 in Thermal Vac
Bus Assembly Probe I&T FM2/FM3 Thermal Vacuum

21 JPL2 PCA Buildup PCA Assembly and Test

22 FM2/FM3 Thermal Vacuum JPL2 Environments Acoustics & Shock Vibration
Spin Balance Thermal Vacuum FM2/FM3 Thermal Vacuum Storage

23 Solar Array Illumination
ASO Probe Processing Delivery to ASO Bolt Cutter Installation Performance Tests Solar Array Illumination

24 ASO Probe Fueling Vibration Acoustics Spin Balance
Dry Weigh & Pressurize Fueling Thermal Vacuum Storage

25 ASO PCA Processing Final checks Acoustics Spin Balance PCA Integration
SSS Installation Ready for Probes Vibration Fairing Installation Spin Balance Storage

26 Ground Based Observatories
Production UCB Fort Yukon, AK, site GMAG ASI EPO GMAG

27 Flight Profile

28 Mission Profile 81

29 Coast Placement Tail 1 Orbit Plans http://sscweb.gsfc.nasa.gov/tipsod/

30 Probe Placement Decision
Assigned Constellation IDs (P1−P5) to Probe Buses THEMIS A −> P5 THEMIS B −> P1 THEMIS C −> P2 THEMIS D −> P3 THEMIS E −> P4 Decision Based on Probe Bus and Instrument Performance Also Included Performance Details Found During Ground Testing Only Differences Noted Are in Telecom System Team Members Involved in Probe Placement Decision PI, PM, MSE, MOM, MDL, Swales Probe Bus Systems Lead, Instrument Scientists, GSFC Program Manager and GSFC Project Scientist

31 Year at a Glance Predicted conjunctions exceed 188hrs/season with ~50% margin

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