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

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

ILWS-2011

First SPECTR-R orbitst

ILWS-2011

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 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

Small satellite platform MKA KARAT for scientific projects

5 spacecraft are contracted for 2010-2015up to 60 kg of payload

First launch in 2011

ILWS-2011

2011 MKA-1: Zond-PP (microwave remote sensing)……

2014-2015 MKA-4: Strannik (magnetospheric)

2015-2016 MKA-5: ARKA (high resolution solar corona)