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THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canavera

THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

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Page 1: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

THEMIS and ARTEMIS

David G. Sibeck

THEMIS Project Scientist

NASA/GSFC

2/17/2007Cape Canaveral

Page 2: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Outline

• Substorms

• NASA’s THEMIS mission • Recent results

• Status and Future plans

Page 3: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Earth’s Magnetosphere

SW

Earth’s dipole magnetic field carves out a cavity in the oncoming supersonic solar wind

.. . . . JB

B

Page 4: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Solar Wind Pressure Variations

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Variations in the solar wind dynamic pressure (nMV2) buffet the magnetosphere,

Page 5: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

But the IMF Orientation Controls the Interaction…

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…which generally turns out to be unsteady….

Page 6: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Our own Dedicated Array of THEMIS Ground Observatories Shows Just how Unsteady!

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Page 7: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Themis Mission Objective:Distinguish Between Two Substorm Models …

Current Disruption Reconnection(a) Near Earth Initiation (b) Mid-Tail InitiationEIct.V. VPlasma process on auroral field line causescurrent disruption (CD) and substorm current wedgeAn X-type magneticneutral line formsat a CD siterarefaction wave causes CDto spread tailward

Multiple CD sites1 2

34 Substorm current wedge3 Braking & dawnward current

High-speed flow NENL124

Implosion near Earth

Equatorward arc brightens

Explosion far from Earth

Poleward arc brightens

Page 8: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Flows

?Rarefaction wave

?

P2P3

P4P5

GBOP1

THEMIS Mission Objective: Pinpoint When, Where, How

Energy Stored in Magnetotail is Released

First distant magnetotail and poleward arcOr

First near magnetotail and equatorward arc?

Page 9: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

SPACECRAFT AND INSTRUMENTS

SST

ESAEF

IaEFIs

FGM

SCM

Tspin=3s

FIVE IDENTICALLY-INSTRUMENTEDSPACECRAFT (128 kg), EACH CARRYING:

ESA: Electrostatic analyzer measures0.003-30 keV ions/electrons (UCB)

SST: Solid state telescopes measures0.03-6 MeV ions and electrons (UCB)

FGM: Fluxgate magnetometer measures magnetic field to 128 Hz (Germany)

SCM: Search coil magnetometer measures 0.001 - 4 kHz magnetic field (France)

EFI: Electric field instrument on wires andaxial booms 0.0003 - 400 kHz (UCB)

Page 10: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

5 THEMIS SpacecraftLine Up Once/4 Days in Tail

Sun

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Page 11: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Case study addressed our primary objective:

Argued that distant tail reconnection triggerssubstorm onset (not vice-versa)

•Vassilis Angelopoulos et al. [2008]

“I see flows consistent with reconnection in thedistant tail followed by auroral brightening,currents, and pulsations at the ground, and thendipolarization in the near-Earth tail. Thisindicates reconnection drives substorms“

…but see comment [Lui, 2009], reply [Angelopoulous, 2009]

Page 12: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Magnetic FieldB(nT)δ Z

Flow( / )V km s Z

AuroralIntensity

( )Relative Units

1P

2P

3P

Magnetic Field( )B nTδ Z

Flow( / )V km s Z

Magnetic Field( )B nTδ Z

Flow( / )V km s X

TRx

TAI

TCD3rd

1st

2nd

P2 P1P3P4

P5 T=0Rx

x

X [R]GSM E

Z

[R]

GSM

E

T=182sCD

T=96sAI

Magnetotail

Earth

ToSun

3rd

1st

2nd

Timing of ground and space:

Vz

Vz

123

TIMELINE

Time the wiggles and demonstratetheir sense is consistent withreconnection. What about arcs?

?

Page 13: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

If the substorm begins far from Earth, why does the most equatorward arc (mapping to near Earth) often appear to brighten

first? Nishimura et al. [2009] argue that it doesn’t!

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1 Initial Brightening

2

3 Equatorward arc

Page 14: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

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Nishimura et al. propose this model to resolve contradiction

Aurora Feature Magnetotail Feature1 Poleward boundary intensifies Reconnection begins in distant tail

2 N/S arc moves equatorward Earthward flow

3 Contact with existing arc Contact with near-Earth plasma sheet

4 Azimuthal drift along growth phase arc

Azimuthal drift in response to increasing pressure gradient

5 Breakup Instability in near-Earth tail

Out

In

Hi-Lat

Low-Lat

Page 15: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

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[Runov et al., 2009]

Earthward-moving

Observations prompt SimulationsEarthward

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Match old MHD simulations [Hesse et al., 1998] and prompt new full particle simulations [Sitnov et al., 2009]

Page 16: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Pc1 Waves Propagate OutwardFrom Footprint on the Ground

Model Observations

Audience: Please HelpRemind Speaker To Show MovieNOW!

Magnetoseismology with Pc 1 (1 Hz) Waves [Rae et al., 2009 Spring AGU Press Release]

Page 17: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Direct Evidence for Magnetic Field Lines Resonating at Individual Frequencies

Multiple spacecraft validate themagnetic field line resonance model[Sarris et al. Feb 2009]:

Disturbances cause each field line to oscillate at its own natural frequency, determined by its length and the mass it carries

1-30 mHz

Page 18: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

What Comes Next?THEMIS and ARTEMIS

P1=TH-BP2=TH-CP3=TH-DP4=TH-EP5=TH-A

Daily orbits,

new interspacecraft

separations in

meridional plane

Lissajous andLunar orbits

Page 19: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

How ARTEMIS Reaches the Moon

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Page 20: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

What ARTEMIS will do at the MoonFor Heliophysics

• When Moon is in the Magnetosphere:– Reconnection, particle acceleration, turbulence

• When Moon is in the Solar Wind:– Reconnection, particle acceleration, turbulence

• Near the Moon:– Lunar wake, electric fields, particle acceleration

Page 21: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

If Planetary has funding, ARTEMIS will optimize orbits and operations to study….

• Dust Levitation in Electric Fields:– Monitor input and study lunar electric field – Use reflectometry to study surface electric field– Provide local electric field, particles to LADEE

• LADEE dust detector detects response to input

• Lunar Exosphere– Composition, distribution of:

• exospheric ions• sputtered ions• regolith

– Exospheric variations with solar activity, cycle

• Lunar Surface and Interior– Crustal magnetic fields– Conductivity depth profile– Surface charging

P1P1P2P2

LADEELADEE

Exospheric orSputtered ions

Secondary and photo-electronsreveal regolith properties

Core?

P2P1 Conductivity

Page 22: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

ARTEMIS and Exploration

• First operational use of Lunar Lissajous orbits (LL1 & LL2), useful for:– Staging lunar landings– Positioning communications relay stations at the moon(Station-keeping requirements thus far unknown)

• ARTEMIS’s 6 month residence in LL1&LL2 provides:– Good estimate of station-keeping fuel requirements – Proof of operational requirements (frequency/magnitude of thrusts) needed– Rapid transition of knowledge to NASA centers for future planning

LL1 LL2

~12

0000

km

To Earth

Moon

TOP VIEW

SIDE VIEW

Moon

Page 23: THEMIS and ARTEMIS David G. Sibeck THEMIS Project Scientist NASA/GSFC 2/17/2007 Cape Canaveral

Summary• THEMIS

– A mission to determine the cause of geomagnetic substorms employing 5 S/C and a dedicated array of ground observatories…

– Case studies addressing primary objective completed, statistical studies underway!

• Recent results from the extended THEMIS mission– Working on reconciling conflicting substorm observations

• Future plans– Outer two THEMIS spacecraft go to the Moon: ARTEMIS– Inner three THEMIS S/C continue core mission

All data public: Need your help analyzing!