Download CORONAS-F Institute of Terrestrial Magnetism, Ionosphere and

Russian magnetospheric &
heliospheric missions
Space Research Institute
CORONAS-PHOTON
Solar imaging and spectroscopy from EUV to 2000 MeV
To be launched in fall 2008
Currently flight payload is
delivered.
Completion of satellite
Preparation is expected in August
Moscow Engineering
Physics Institute
Yu. Kotov
http://iaf.mephi.ru
Space Research Institute
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.
Project Scientist: G.N.Zastenker
[email protected]
Targets:
Fine-scale solar wind, IMF, SCL
up to 32 samples/sec
Solar wind, IMF, SCL monitoring
Space Research Institute
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, Greece
geometric factor ~ 1
electrons 15-350 keV
ions 15- 3200 keV
PI: K. Kudela, IEP, w/part DUTH/SSL, IKI
Data management system SSNI-2 – Russia
100 GB onboard memory
possibility of intelligent data handling and compression
PI: L. Chesalin, IKI
Space Research Institute
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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
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
Space Research Institute
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RESONANCE 1А и 1В
~ 1-10 km
~1000- 5000
~ 5000-15000
RESONANCE 2А и 2В
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Space Research Institute
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Space weather-related
Ring current and outer radiation belt dynamics
Plasmasphere & plasmapause dynamics
Magnetospheric cyclotron maser
Interaction of electrons and waves
Auroral region processes
small scale acceleration zones
Space Research Institute
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Launch 2012: will operate with
• Radiation Belt Storm Probes by NASA LWS
• ERG
• ORBITALS
ILWS inner magnetosphere constellation in 2012 ?
Space Research Institute
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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
Space Research Institute
Mini-spacecraft for magnetospheric science
Possible collaboration with future MMS / X-scale projects
Sci payload weight ~ 40 kg
Space Research Institute
Interhelioprobe
Launch 2014.
In fall 2008 decision to start phase B will be taken.
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
Space Research Institute
INTERHELIOPROBE
Start
from
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Earth
Inclination of the orbit
Multiple
Venus
Flight-by
Space Research Institute
INTERHELIOPROBE
High 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.
Space Research Institute
INTERHELIOPROBE
In - situ measurements near the Sun
Distribution function. Remnants of coronal heating and
related plasma processes.
Wave-particle interactions.
Beams. Temperature anisotropy.
Radio emission. Neutrons.
Space Research Institute
INTERHELIOPROBE
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
Space Research Institute
INTERHELIOPROBE in Aphelion
Space Research Institute
Interhelioprobe & Solar Orbiter
RSA
&
ESA
2014
A joint IZMIRAN & IKI Project
Contact: Prof. Kuznetsov, IZMIRAN
[email protected]
Space Research Institute