RUSSIAN SPACE MISSIONS FOR SOLAR-TERRESTRIAL SCIENCE ILWS-2011 A.A. Petrukovich, L.M. Zelenyi Space Research Institute V.D. Kuznetsov IZMIRAN.

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Presentation transcript:

RUSSIAN SPACE MISSIONS FOR 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 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, Greece geometric factor ~ 1 electrons keV ions keV PI: K. Kudela Data management system SSNI-2 – Russia 40 GB onboard memory intelligent data handling and compression PI: L. Chesalin ILWS-2011

First SPECTR-R orbits t

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

ILWS-2011 Main engine Phobos module microsat Sample return module

ILWS-2011 Sample return module microsat

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

ILWS-2011

RESONANCE ILWS-2011 To be launched in : 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 km Period: 8 hours Apogee: ~27000 km Inclination: 63.4 o Co-rotation with magnetic line at L~4-5

RESONANCE-HAARP  Artificial of electromagnetic waves  Modification of precipitation particles  Modification of the reflection coefficient from the ionosphere ILWS-2011

RESONANCE instruments Electric and magnetic sensors Wave analyzer and interferometer DC – 10 MHz Plasma sensors Cold plasma Suprathermal plasma Energetic particles Relativistic electrons

International inner magnetospheric constellation RESONANCEaltitude km inclination 63 deg ERG 4-5 Re near-equatorial RBSP 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 : Draft design study ILWS-2011

Redesign of Interhelioprobe orbit Inclination of the orbit Heliospheric distances ILWS-2011 Perihelion ~70 Rs Fast inclination change

SOLAR INSTRUMENTATION Optical photometer Magnetograph Chemical Composition Analyzer EUV Imager-Spectrometer Coronograph X-ray Imager Heliospheric Imager X-ray Polarimeter Gamma-Spectrometer HELIOSPHERIC INSTRUMENTATION Solar Wind Ion Analyzer Solar Wind Electron Analyzer Solar Wind Plasma Analyzer Magnetic Wave Complex Magnetometer Energetic Particle Telescope Neutron Detector Radio Spectrometer Payload ILWS-2011  Power: 120 W  Telemetry: 120 kb/s  Mass: 120 kg

Solar Orbiter ESA Cooperation of Interhelioprobe with Solar Probe / Solar Orbiter ILWS-2011 Interhelioprobe Solar Probe+ Interhelioprobe Solar Orbiter Orbital conjunctions in and out of ecliptic

Small satellite platform MKA KARAT for scientific projects 5 spacecraft are contracted for up to 60 kg of payload First launch in 2011 ILWS MKA-1: Zond-PP (microwave remote sensing) … MKA-4: Strannik (magnetospheric) MKA-5: ARKA (high resolution solar corona)