Post on 30-Dec-2015
RUSSIAN SPACE MISSIONSFOR SOLAR-TERRESTRIAL SCIENCE
ILWS-2011
A.A. Petrukovich, L.M. Zelenyi
Space Research Institute
V.D. Kuznetsov
IZMIRAN
Launched in February 2011
Solar and magnetospheric payload:
Cosmic ray
Energetic plasma
Magnetic field
Solar radiation
Geostationary meteo spacecraft ELECTRO-L
ILWS-2011
smdc.sinp.msu.ru
Radioastronomy mission SPECTR-R
space VLBI
10-meter radio telescope
orbit with apogee 350 000 km
PLASMA-F : payload of opportunity
solar wind, IMF, SCR up to 32 samples/sec
ILWS-2011
Launched in July 2011
PLASMA-F instruments
Magnetic field instrument MMFF – Russia, Ukraine 2 DC magnetometers 2 AC magnetic sensors (10 Hz – 100 kHz)
PI: A. Skalsky
Fast solar wind monitor BMSW - Czech R., Russia, China 6 Faraday cups with possibility of instantaneous solar wind velocity vector and density determination
PI: Y. Safrankova
Energetic particle instrument MEP2 – Slovakia, Greecegeometric factor ~ 1electrons 30-350 keVions 30- 3200 keV
PI: K. Kudela
Data management system SSNI-2 – Russia 40 GB onboard memoryintelligent data handling and compression
PI: L. Chesalin
ILWS-2011
PHOBOS sample return mission PHOBOS-GRUNT
Plasma payload:
Ion and neutral spectrometry
Magnetometer
Chinese microsatellite
ILWS-2011
To be launched in November 2011
Ionospheric micro satellite CHIBIS - M
Microsat to study
atmospheric electricity and TGFs
spacecraft packed and waiting transfer to ISS in october-december 2011
X-ray / gamma detector
UV sensor
Radiowave analyzer
Magnetic and electric sensors
Photocamera
Data analysis system
ILWS-2011
To be launched in fall 2011
RESONANCE
ILWS-2011
To be launched in 2014
2011: Engineering models delivery
Inner magnetospheric mission
Two pairs of spacecraft
Magneto-synchronous orbit
Space weather Ring current, outer radiation belt,plasmasphere
Magnetospheric cyclotron maser Interaction of electrons and waves
Auroral region acceleration Small-scale active zones, precipitation
Two pairs of spacecraft
ILWS-2011
Distance in pairs: varies from 1-10 km to 100-1000 km
Period: 8 hours
Apogee: ~27000 km
Inclination: 63.4o
Co-rotation with
magnetic line at L~4-5
ILWS-2011
RESONANCE instruments
Electric and magnetic sensorsWave analyzer and interferometer
DC – 10 MHz
Plasma sensorsCold plasmaSuprathermal plasmaEnergetic particles Relativistic electrons
International inner magnetospheric constellation
2012-2015
RESONANCE altitude 27000 km inclination 63 deg
ERG 4-5 Re near-equatorial
RBSP 30000 km near-equatorial
+ geostationary satellites, MMS, THEMIS, KUAFU-auroral
Collaborative science topics in which synergy is possible ? Orbital conjunctions ?
ILWS-2011
Interhelioprobe
Solar observations from inner heliosphere
High-resolution observations of the solar atmosphere
In-situ measurements near Sun
Out-of-ecliptic observations
Observations of Sun invisible side To be launched in 2017-2018
2011: Draft design study
ILWS-2011
Redesign of Interhelioprobe orbit
Inclination of the orbitHeliospheric distances
ILWS-2011
Perihelion ~70 Rs
Fast inclination change
SOLAR INSTRUMENTATIONOptical photometerMagnetograph Chemical Composition AnalyzerEUV Imager-SpectrometerCoronographX-ray ImagerHeliospheric ImagerX-ray PolarimeterGamma-Spectrometer
HELIOSPHERIC INSTRUMENTATIONSolar Wind Ion Analyzer Solar Wind Electron Analyzer Solar Wind Plasma Analyzer Magnetic Wave Complex Magnetometer Energetic Particle TelescopeNeutron DetectorRadio Spectrometer
Payload
ILWS-2011
Power: 120 W Telemetry: 120 kb/s Mass: 120 kg
Solar OrbiterESA
Cooperation of Interhelioprobe with Solar Probe / Solar Orbiter
ILWS-2011
Interhelioprobe
Solar Probe+ Interhelioprobe
Solar Orbiter
Orbital conjunctions in and out of ecliptic