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Russian magnetospheric & heliospheric missions

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CORONAS-PHOTON

Solar imaging and spectroscopy from EUV to 2000 MeV

To be launched in fall 2008

Moscow EngineeringPhysics Institute

Yu. Kotov

http://iaf.mephi.ru

Currently flight payload is delivered. Completion of satellite Preparation is expected in August

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Solar-terrestrial payload onboard SPECTR-R

• space VLBI project.

• 10-meter radio telescope

• orbit with apogee 350 000 km

• launch in late 2008 or 2009

• Currently main flight payload is under integration test

PLASMA-F is solar-terrestiral payload of opportunity onboard SPECTR-R.

will be delivered after competion of main payload tests.

Targets: Fine-scale solar wind, IMF, SCL

up to 32 samples/sec

Solar wind, IMF, SCL monitoring

Project Scientist: G.N.Zastenker gzastenk@iki.rssi.ru

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PLASMA-F instruments

Magnetic field instrument MMFF – Russia 2 DC magnetometers 2 AC magnetic sensors (10 Hz – 100 kHz)

PI: A. Skalsky, IKI, w/part LSC

Fast solar wind monitor BMSW - Czech R., China 6 Faraday cups with possibility of instantaneous solar wind velocity vector and density determination

PI: G. Zastenker, IKI, w/part ChU, CSS

Energetic particle instrument MEP2 – Slovakia, Greecegeometric factor ~ 1electrons 15-350 keVions 15- 3200 keV

PI: K. Kudela, IEP, w/part DUTH/SSL, IKI

Data management system SSNI-2 – Russia 100 GB onboard memorypossibility of intelligent data handling and compression

PI: L. Chesalin, IKI

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Investigation of wave-particle interactions and plasma dynamics in the inner magnetosphere

Space Research Institute, Moscow Institute of Applied Physics, N.Novgorod

European participation

RESONANCE RRESO NANCEРЕЗО Н АН С

Magnetosynhronous orbit

Apogee: ~30 000 km,Perigee: ~ 1 800 km,Inclination: + and - 63.4o (two S/C)

Co-rotation magnetic tube: up to 3 hours

Launch: 2012 on schedule

Currently change from 2x300 kg to 4x150 kg satellites is considered.

http://resonance.romance.iki.rssi.ru

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RESONANCE 2А и 2В

RESONANCE 1А и 1В

~ 1-10 km

~1000- 5000

~ 5000-15000

RRESO NANCEРЕЗОН АН С

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RESONANCE RRESO NANCEРЕЗОН АН С

Space weather-related

Ring current and outer radiation belt dynamics

Plasmasphere & plasmapause dynamics

Magnetospheric cyclotron maser Auroral region processes

  Interaction of electrons and waves small scale acceleration zones

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RESONANCE RRESO NANCEРЕЗО Н АН С

Launch 2012: will operate with

• Radiation Belt Storm Probes by NASA LWS

• ERG

• ORBITALS

ILWS inner magnetosphere constellation in 2012 ?

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Small satellite platform KARAT for scientific projects

Dry weight ~ 100 kg plus up to 60 kg of payload

First launch in 2009

Later used in Resonance, etc

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Mini-spacecraft for magnetospheric science

Possible collaboration with future MMS / X-scale projects

Sci payload weight ~ 40 kg

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MAIN SCIENTIFIC GOALS

mechanisms of the coronal heating and solar wind

fine structure and dynamics of the solar atmosphere

origin and the global dynamics of solar flares and CMEs

generation and propagation of solar energetic particles

mechanism of the solar dynamo and solar cycle

high latitudes studies

InterhelioprobeInterhelioprobe

Launch 2014. In fall 2008 decision to start phase B will be taken.

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Start from the Earth

INTERHELIOPROBE

MultipleVenus Flight-by

Inclination of the orbit

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INTERHELIOPROBEINTERHELIOPROBEHigh resolution observationsHigh resolution observations

Fine structure and dynamics of solar atmosphere:magnetic network;magnetic flux elements; turbulence.

Supergranulation and its role in large-scale dynamics of magnetic field and corona

Small-scale magnetic activity:loops dynamics and motions of its footpoints, microflares, reconnection.

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INTERHELIOPROBEINTERHELIOPROBE

In - situ measurements near the SunIn - situ measurements near the Sun

Distribution function. Remnants of coronal heating and related plasma processes.

Wave-particle interactions.

Beams. Temperature anisotropy.

Radio emission. Neutrons.

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SOLAR INSTRUMENTATION

Optical telescope Magnetograph X-ray imager-spectrometer Coronograph

HELIOSPHERIC INSTRUMENTATION

Solar Wind Ion Analyzer Solar Wind Electron Analyzer   Solar Wind Plasma and Dust Analyzer Magnetic Wave Complex      Magnetometer     Energetic Particle Telescope Neutron Detector Radio Spectrometer Detector

Mass: 100 kg Power: 100 W Telemetry: 100 kb/s

INTERHELIOPROBE

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INTERHELIOPROBE in AphelionINTERHELIOPROBE in Aphelion

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A joint IZMIRAN & IKI Project

Contact: Prof. Kuznetsov, IZMIRAN

kvd@izmiran.ru

Interhelioprobe & Solar OrbiterInterhelioprobe & Solar OrbiterRSA & ESARSA & ESA

20142014