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FEDERAL SPACE AGENCY

FUNDAMENTAL FUNDAMENTAL SPACE SPACE RESEARCHRESEARCHWIDE FIELD FOR WIDE FIELD FOR

COOPERATION BETWEEN COOPERATION BETWEEN INDIA AND RUSSIAINDIA AND RUSSIA

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MAIN AREAS OF FUNDAMENTAL SPACE RESEARCH IN RUSSIAMAIN AREAS OF FUNDAMENTAL SPACE RESEARCH IN RUSSIASpace plasma and the Solar physics:

Internal heliosphere and close-range Sun researches; Studies of resonance interaction between electromagnetic radiation and charged particles of the Earth's magnetosphere; Studies of earthquakes' forerunners.

Exo-atmosphere astronomy: High-accuracy astrometry measurements and precise definition of fundamental coordinate system; Astronomic objects observation in radio, ultraviolet, gamma, X-ray, millimeter and sub-millimeter ranges of spectrum.

Planet and small bodies of the Solar System researches: Studies of atmospheres, magnetosphere and surfaces of the Solar System planets; Expansion of the Solar System's small bodies researches, including the delivery of the Phobos ground samples to the Earth.

Basic problems of space biology, physiology and medicine:• Carrying out research programs on study of microgravity and other spaceflight factors influence on processes of biological objects adaptation.

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MAIN AREAS OF FUNDAMENTAL SPACE RESEARCH IN RUSSIAMAIN AREAS OF FUNDAMENTAL SPACE RESEARCH IN RUSSIA

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SCIENTIFIC AREAS SOME PROJECTS IN DEVELOPMENT

Space plasma and the Solar physics Coronas-Photon, Resonance, Intergelio-Zond

Outer atmosphere astronomy World Space Observatory

Planetary and the Solar System's small bodies research

Phobos-Grunt, Luna-Glob

Basic problems of space biology, physiology and medicine

Bion-M

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SOLAR PHYSICS, SOLAR PHYSICS, STUDIES ON SOLAR-STUDIES ON SOLAR-TERRESTRIAL LINKS TERRESTRIAL LINKS AND PROCESSES IN AND PROCESSES IN

MAGNETOSPHERE OF MAGNETOSPHERE OF THE EARTH THE EARTH

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INDIA PARTICIPATES IN INDIA PARTICIPATES IN THE RUSSIAN THE RUSSIAN

CORONAS-FOTON CORONAS-FOTON PROJECTPROJECT

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CORONAS-PHOTONCORONAS-PHOTON

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MagnetometerPINGUIN

KONUS-RF

RT-2/GN-2M

RT-2/GA

RT-2/S

SUN

STEP-F

PHOKA

TESIS

KONUS-RF-anti

Pressure-module

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CORONASCORONAS--PHOTONPHOTON projectto study space plasma and the Solar physics (launching date - 2007)

Main objectives of the mission Study of hard electromagnetic radiation dynamic in a wide energy range from EUV to 2000MeV; Nuclear gamma-lines spectroscopy of Solar activity regions; Detection of solar neutrons with energies higher 20MeV; Study of linear polarization and variability of hard X-ray emission; Monitoring of the Solar EUV, soft and hard X-ray emissions; Charge particle environment measurements; Simultaneously astrophysical observation including gamma-ray bursts; Monitoring of Earth upper atmosphere in EUV and soft X-rays radiated by the quite Sun.

Main characteristics of the spacecraft Mass of the satellite - 2520 kg Mass of the scientific payload - 700 kg Orbit: circular, 500 km height, inclination – 82,5 Nominal mission lifetime - 3 years (extended 5 years)

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FEDERAL SPACE AGENCY

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THERE ARE THERE ARE OPPORTUNITIES FOR OPPORTUNITIES FOR

COOPERATION WITHIN COOPERATION WITHIN THE FRAMEWORK OF THE FRAMEWORK OF

OTHER RUSSIAN OTHER RUSSIAN PROJECTSPROJECTS

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RESONANCE projectRESONANCE projectMain goals:

Long-term observations of the natural phenomena, localized in the selected flux tube:  -  Dynamics of magnetospheres cyclotron maser,  -  Ring current formation,  -  Refilling of plasmosphere after magnetic storms,  -  Study of the role of the small-scale phenomena in the global plasma dynamics. An artificial influence on the operation of magnetospheric maser. Basic options:  -  Artificial excitation and/or stimulation of wave modes;  -  Modification of the flux of precipitating particles;  -  Variation of maser Q-factor by the modification of reflection index in the ionospheric footprint of the selected magnetic flux tube.

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

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RESONANCE projectRESONANCE project

Two Spacecrafts location under the faring of “Dnepr” launch vehicle

Main parameters:

Altitude of perigee 1000 kmAltitude of apogee 21000 kmInclination 62,80

Orbital period 6,4 hourWeight of the satellite 550 kgWeight of the scientific payload 150 kg

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INTERHELIOPROBE INTERHELIOPROBE projectproject

1 – whitelinght imager, 2- coronograph, 3 – neutron analyzer, 4 – solar gamma-

spectrometr, 5 – plazma analyzer, 6 – magnetometr, 7 – energetic

particle detector, 8 – radiospectrometr, 9 – dust detector, 10 – magnetic sensor

ULF/VLE, 11 – solar protective screen, 12 – solar panel,

13 – astroinstrument, 14 – scientific payload bay, 15 –

high-gain antenna, 16 – radiospectrometr antenna, 17 – solar protective screen control

MAIN SCIENTIFIC GOALS• to identify mechanisms of the coronal

heating and solar wind;• to investigate the fine structure and

dynamics of the solar atmosphere;• to determine the origin and study the

global dynamics of the most powerful solar activity phenomena (solar flares and CMEs) and their influence on the heliosphere and space weather;

• to investigate generation and propagation of solar energetic particles;

• to observe from high latitudes and to investigate the solar atmosphere and corona in the polar and equatorial regions;

• to determine the mechanism of the solar dynamo and solar cycle.

Project of investigation the Sun and Inner Heliosphere

Interhelioprobe SC with deployed scientific complex

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FEDERAL SPACE AGENCY

SOLAR INSTRUMENTATION• OPTICAL TELESCOPE• MAGNETOGRAPH• X-RAY IMAGER-SPECTROMETER• CORONAGRAPH

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 • Electron Gun

Ballistic scenario of the mission• multiple gravity-assisted maneuvers near

the planet Venus (VGMs); • electric propulsion low thrust system (in

conjunction with VGMs).

Mission phases• cruise phase (Earth-Venus); • ecliptic phase (co rotation); • out-of-ecliptic phase (increase of orbit

inclination up to 30-380 with respect to solar equatorial plane);

• perihelion lowering on inclined orbit (as possible).

INTERHELIOPROBE INTERHELIOPROBE projectproject

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ASTROPHYSICSASTROPHYSICSAND COSMIC RAYS AND COSMIC RAYS

PHYSICS PHYSICS

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World Space World Space ObservatoryObservatory

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Scientific Objectives:Orbital ultraviolet observatory will study following phenomena and problems: Chemical evolution of gas in the Universe; Physical and chemical properties of photo-ionized gas; Detailed study of the properties of a well defined sample of local and moderately distant (z~1) star forming galaxies in UV as a step toward physical interpretation of the spectra of galaxies at moderate resolution from very large telescope at high red-shift; Chemical abundance of stars; Physical process of a wide range outflow phenomena, in conjunction with space missions in the X-ray band; Searching of new phenomena by observing spectroscopically peculiar objects discovered by the ground spectroscopic survey.

Outer atmosphere astronomy, Outer atmosphere astronomy, World Space ObservatoryWorld Space Observatory

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EXPLORATION OF EXPLORATION OF SOLAR SYSTEM SOLAR SYSTEM

PLANETS AND MOONPLANETS AND MOON

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PHOBOS-GRUNTPHOBOS-GRUNT

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Planetary and the Solar System's small bodies research, project PPHOBOSHOBOS-G-GRUNTRUNT

Goals of the Mission-Phobos: regolith sample return, Phobos in situ study, Mars and Phobos remote sensing.Scientific Objectives: study physical and chemical characteristics of Phobos regolith and subsurface layers in situ and under laboratory conditions; study of the role played by asteroidal impacts in the formation of terrestrial planets, in the evolution of their atmospheres, crusts, and inventories of volotiles; study of the origin of the Martian satellites and their relation to Mars; search of possible paleolife; study of peculiarities of orbital and proper motion of Phobos; study physical conditions of the Martian environment (dust, gas, plasma components); Monitoring of dynamic of the Martian atmosphere and seasons climate changing.Launch - October 2009Earth – Mars flight duration - 10 – 11,5 monthsReturn rocket launch from Phobos - July-August 2011Mars – Earth flight duration - 11,5 monthsEarth arrival - June-July 2012Total mission duration ~ 33-34 months

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FEDERAL SPACE AGENCY

THERE IS AN OPPORTUNITY TO THERE IS AN OPPORTUNITY TO DELIVER AN INDIAN SMALL DELIVER AN INDIAN SMALL

INTERPALNETARY SPACECRAFT INTERPALNETARY SPACECRAFT TO THE ORBIT AROUND MARS.TO THE ORBIT AROUND MARS.RUSSIA IS READY TO ASSIST IN RUSSIA IS READY TO ASSIST IN

ITS IMPLEMENTATIONITS IMPLEMENTATION

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R U S S I A N F E D E R A T I O NR U S S I A N F E D E R A T I O N

FEDERAL SPACE AGENCY

DUE TO THE STRICTLY FIXED DUE TO THE STRICTLY FIXED ASTRONOMICAL DATE OT THE ASTRONOMICAL DATE OT THE MISSION LAUNCH AN INTER-MISSION LAUNCH AN INTER-

AGENCY AGREEMENT AGENCY AGREEMENT REGARDING THE CONCLUSION REGARDING THE CONCLUSION

OF THE CONTRACT MUST BE OF THE CONTRACT MUST BE SIGNED BY THE END OF 2005SIGNED BY THE END OF 2005

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LUNA-GLOB LUNA-GLOB MISSIONMISSION

Main goals of mission

Spacecraft LUNA-GLOB consist of: 10 small Penetrators (Vent 2,6 km/sec); 3 big Penetrators (Vent 100 m/sec); descent vehicle

Launcher – “Dnepr”, Data of launch - 2012

Scientific objectives of mission:

Investigations of lunar inner structure; Intelligence lunar natural resources; Study influence particles and electromagnetic radiation on lunar surface; Determination of the volatile components in south pole crater of moon.

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LUNA-GLOB LUNA-GLOB MISSION. MISSION. MISSION MISSION PROFILEPROFILE

Operation on the orbit ofthe Moon Artificial satellite

Insertion with the help of APS intothe Earth-Moon flight trajectory

Carrying out of trajectory measurements on the parking near-Earth orbit

Separation of the APSdroppable tank’s unit

APS separationInsertion into the orbit

of the Moon satellite

Braking with the help of the APS

Spacecraft reorientation, correction.Spinning and separation of the third landing vehicle

Spacecraft reorientation, correction.Spinning and separation of cassette with small penetrators

Spacecraft reorientation, correction.Spinning and separation of the first landing vehicle

Spacecraft reorientation, correction.Spinning and separation of the second landing vehicle

Correction, eliminating

errors of insertion Insertion with the help of autonomous propulsion system

(APS) into the parking orbit

Launch

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RESEARCHES IN FIELD RESEARCHES IN FIELD OF SPACE BIOLOGY, OF SPACE BIOLOGY,

PHYSIOLOGY AND PHYSIOLOGY AND MEDICINE MEDICINE

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BION-M / BIOCOSMOSBION-M / BIOCOSMOS

R U S S I A N F E D E R A T I O NR U S S I A N F E D E R A T I O N

FEDERAL SPACE AGENCY

Objectives:Carrying out fundamental and application

researches in field of space biology and

medicine, radiation-physical and radiation-

biological experiments in favor of manned

spaceflights (with different durations and

complexity degrees) medical and biological

problems solution.

Planned flightsPlanned flights: 2010, 2013 : 2010, 2013 andand 2016 2016

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““BION-M”: MAIN PERFORMANCESBION-M”: MAIN PERFORMANCES

Developer «TsSKB-Progress» (Samara)

Working orbit parameters: maximal height minimal height inclination

394 km266 km

62,8о

Maximal mass of spacecraft 6300 kg

Payloads mass Mass of Payloads inside descent vehicle Mass of Payloads outside descent vehicle

от 850 до 1200 kgUp to 700 kg Up to 200 kg

Duration of orbital flight Up to 45 days (+ 1 day reserve)

Mode of flight Non-oriented

Payloads average power consumption No greater than 350 W

Microgravity level 10-5 - 10-6  gо

Launcher “Soyuz”

Launching pad Baikonur

Delivery to Earth of experiments results:

Inside descent vehicle with soft landing Value of velocity vertical component at landing – not greater than 5 m/s

Via radio-telemetry downlink On receiving ground stations, which are situated on Russian territory

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““BION-M” MISSIONS:BION-M” MISSIONS: OBJECTS UNDER STUDY AND FACILITIESOBJECTS UNDER STUDY AND FACILITIES

• Rats

• Monkeys

• Reptiles• Amphibia

• Microorganisms• Insects• Worms• Cultures of cells and tissues

• Fishes

• Plants• Eggs of birds

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FEDERAL SPACE AGENCY

FUTURE RESEARCHES OBJECTIVES:

• Study of dependence of structural, metabolic and functional changes in organism upon duration of stay in microgravity.

• Biological effects due to combining influence from microgravity and cosmic rays onto organism.• Organism ability to counteract pathogenic microorganisms and toxins.• Particularities in healing of skin wounds, bones and muscles traumatic damages. • Pharmacokinetics and pharmacodynamics.• Long-term effects of spaceflights. • Molecular and cellular reactions of organisms on spaceflights factors. • Mechanisms of osteogeny.• Mechanisms of muscles atrophy.• Mechanisms of cardiovascular system detraining• Mechanisms of locomotor regulation. • Biological effects of artificial gravity.• Testing of new prophylaxis measures (hypoxia, diet, medicines, and so on).

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FEDERAL SPACE AGENCY

The results of fundamental space The results of fundamental space research as all the basic scientific research as all the basic scientific

results belong to the whole results belong to the whole Humanity.Humanity.

Hence, it is advisable to establish Hence, it is advisable to establish wide international cooperation in wide international cooperation in

this fieldthis field

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FEDERAL SPACE AGENCY

In order to coordinate Russian-In order to coordinate Russian-Indian cooperation in fundamental Indian cooperation in fundamental space research it is suggested that space research it is suggested that a joint working group should be a joint working group should be

created.created.

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FEDERAL SPACE AGENCY

THANK YOU THANK YOU FOR FOR

ATTENTIONATTENTION