1 / 25

Frank Admission : Existence of abundant down-to-earth problems of development.

" ….. we must be second to none in the application of advanced technologies to the real problems of man and society, which we find in our country. … - Dr. Vikram A. Sarabhai. Frank Admission : Existence of abundant down-to-earth problems of development.

rio
Télécharger la présentation

Frank Admission : Existence of abundant down-to-earth problems of development.

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. " ….. we must be second to none in the application of advanced technologies to the real problems of man and society, which we find in our country. … - Dr. Vikram A. Sarabhai • Frank Admission : Existence of abundant down-to-earth problems of development. • Prudent assertion : Science &Technology being crucial apparatus for development. • Commitment : Science &Technology for socio-economic benefits in preference to display of grandeur. • Military Superiority • Technological Dominance • Display of Grandeur Indian Space Program is very different. Very deeply rooted to the society SPACE POLICY

  2. The Humble beginning

  3. Application of Space Technology for the benefit of the common man Mandate and Mantra

  4. India today runs and maintains its own space program Remarkable benefits are being provided to the common man in timely & Cost- effective fashion DID IT WORK ?

  5. * ONE OF THE LARGEST DOMESTIC SATCOM • SYSTEMS - Ku, C, S BANDS • * MULTI-PURPOSE : TELECOM, TV, METEOROLOGY • 200 TRANSPONDERS, GLOBAL/DOMESTIC BEAMS INSAT FAMILY INSAT-2C,D INSAT-1 INSAT-3B INSAT-3E GSAT-2 INSAT-2E APPLE INSAT-3D EDUSAT (GSAT-3) INSAT-3A DTH INSAT-2A,B INSAT-4B

  6. COMMUNICATION • Speech Circuits On Trunk Routes • VSAT Connectivity BROADCAST • Television Broadcasting • Direct To Home (DTH) • TV & Radio Networking OTHERS • Mobile Satellite Service • Search and Rescue • Satellite Navigation DEVELOPMENTAL METEOROLOGICAL • Tele-health • Tele-education • Emergency Communication • Meteorological Imaging • Data Collection Platform • Disaster Warning INSAT SYSTEM APPLICATIONS

  7. EduSat Video + Audio Video + Audio Audio 5 Spot Beams in Ku Band 1 National Beam in Ku Band 1 National Beam in Ext C Band (6 Channels) Class Room-2 Teaching-End Class Room-1 TELE EDUCATION

  8. 180 Hospitals • 146 Dist/ Rural Hospitals • 34 Super Specialty Hospitals Reaching the un-reached Referral Hospitals Video Conferencing Health Specialist Centre Cardiology Pathology Video Conferencing Panel of Doctors TELE MEDICINE VIA SATELLITE

  9. 1999 1995/1997 INDIAN IMAGING SYSTEMS 2003 RESOURCESAT-1 LISS3 - 23 M; 4 XS LISS4 - 5.8 M; 3-XS AWIFS - 70 M; 4-XS IRS-1C/1D LISS-3 (23/70M, STEERABLE PAN (5.8 M); WiFS (188M) INSAT-2E CCD (1KM RESOLUTION; EVERY 30 MNUTESS) 1996 2005 1994 IRS-P3 WiFS MOS X-Ray CARTOSAT - 1 PAN - 2.5M, 30 KM, F/A 1999 IRS-P2 LISS-2 IRS-P4 OCEANSAT OCM, MSMR 1988/91 CARTOSAT-2 PAN - 1M IRS-1A/1B LISS-1&2 (72/36M, 4 BANDS; VIS & NIR) 2007 1982 • IMAGING IMPROVEMENTS • 1KM TO 1.0 M RESOLUTION • GLOBAL COVERAGE • APPLICATION-SPECIFIC RS-D1 MEGHA-TROPIQUES SAPHIR SCARAB & MADRAS 1979 BHASKARA

  10. AGRICULTURE & SOIL • Crop Acreage & Production Estimation • Soil & Land DegradationMapping • Watershed Development • Horticulture Mission for North-East • LAND • Landuse/Land Cover Mapping • Wasteland Mapping • Urban Sprawl Studies • Large Scale Mapping • FOREST, ENVIRONMENT, BIO • Forest Cover & Type Mapping • Forest Fire and Risk Mapping • Biodiversity Characterisation • Environmental Impact Studies • WEATHER & CLIMATE • Extended Range Monsoon Forecasting • Ocean State Forecasting • WATER • Potential Drinking Water Zones • Command Area Management • Reservoir Sedimentation • DISASTER SUPPORT • Flood Damage Assessment • Drought Monitoring • Land Slide Hazard Zonation • OCEAN • Potential Fishing Zone (PFZ) • Coastal Zone Mapping EARTH OBSERVATION – APPLICATIONS

  11. A milestone application towards building social infrastructure Implementation and Feedback status • RAJ • 67,775  90 Ground Water Prospect Map with Sites for Recharge • MP • 22,006  90 • CHG • 34,413  93 • Development of spatial information system on ground water covering problem states • More than 90% successrate in drilled sources (more than 2,00,000 in 7 states) • AP • 35,139  93  Wells Drilled  Success Rate (%) • KAR • 34,688  93 • Kerala • 7,730  92 RAJIV GANDHI NATIONAL DRINKING WATER MISSION

  12. ISRO LAUNCHERS

  13. 22 Launch Vehicle Missions TODAY, 2007 Self reliance in launching November 21, 1963 SLV-3 ASLV LAUNCH VEHICLE 46+ 6 Spacecraft Missions PSLV GSLV 10 4 Self reliance in building satellites INSAT-3E 28.09.03 EDUSAT 20.09.04 CARTOSAT-2 10.01.07 KALPANA-1 12.09.02 INSAT-3A 10.04.03 INSAT-2E 03.04.99 INSAT-4A 22.12.05 SATELLITE APPLICATIONS GSAT-2 08.05.03 HAMSAT 05.05.05 INSAT-3C 24.01.02 ARYABHATA 19.04.75 INSAT-3B 22.03.00 CARTOSAT-1 05.05.05 RESOURCESAT-1 17.10.03 TES 22.10.01 IRS-1D 29.09.97 IRS-P4 26.05.99 FOUR DECADES OF INDIAN SPACE PROGRAMME

  14. Chandrayaan-1 India’s First Lunar Mission ASTROSAT SPACE SCIENCE

  15. First Lunar Mission CHANDRAYAAN-1 • The satellite construction is progressing. • The launch is scheduled in 2008

  16. Chandrayaan-1 Mission Objectives • High resolution imaging and chemical and mineralogical mapping of lunar surface to define the process leading to the formation and chemical evolution of moon. • Remote sensing in visible, near Infra Red, low energy X-ray and high energy X-ray regions • Systematic topographic mapping of the whole surface of the moon. • Develop expertise of planning and execution of mission for sending S/C to orbit around moon, this exercise will help for future planetary exploration missions. • To establish capability of planetary data analysis, data archival and dissemination.

  17. Chandrayaan-1 Mission Spin-offs • Realization of Deep Space Network (DSN) • Establishment of Indian Space Science Data Centre (ISSDC) • With the concept of Announcement Of Opportunity (AO) payloads, many space agencies are participating in Chandrayaan-1 • International Co-operation for Space science and Space exploration • Generation of interest among the student Community

  18. Chandrayaan-1 Payloads ISRO Terrain Mapping Camera – ( TMC ) Hyper Spectral Imager – ( HySI-VNIR ) Lunar Laser Ranging Instrument – ( LLRI ) High Energy X-ray payload – ( HEX ) Moon IMPACT PROBE with MSM, Video camera and an altimeter – ( MIP ) Other Space Agencies / Research Institutions Low Energy X-ray (CIXS & SXM): RAL,UK Mini SAR(APL/NASA, USA) SIR-2, Max Plank Inst, Germany Sub Kev Atom Reflecting Analyzer – IRF, swedan; JAXA,Japan; ISAS, Switzerland; SPL, India Radiation Dose Monitor (Bulgaria) – ( RADOM ) Moon Mineralogy Mapper (JPL/NASA,USA) – (M3)

  19. Possible Future Missions • Basically four types of future missions are being envisaged. (These missions are a result of a thought process within the Indian Scientific community and are not Govt. approved ISRO projects yet) • Follow on mission to Moon: Considered time frame- 2011 (Chandrayaan-2) • Asteroid / Comet flyby mission: Possible time frame- 2015 • Mission to Mars :Timeframe- 2019 • Human Mission : Timeframe 2020 • Missions to other planets (Venus, Mercury…Vision beyond 2020)

  20. Chandrayaan - 2 • Mission includes Orbiter and Lander • Remote Sensing instruments • Lander might include robotics, rovers and penetrators. • Preferred landing sites, specific scientific problems and instruments need to be finalized. Far side of the moon, particularly South Pole Aitkin (SPA) basin is a prime candidate. • Considered time frame : 2011 • Possible instruments on the orbiter: • Terrain mapping camera • 400-4000nm hyper spectral Imager • Low energy X-ray spectrometer (CCD-array) • Gamma ray, neutron, alpha spectrometer

  21. Mission to Asteroid • Orbiter mission to a main belt Asteroid / Comet OR • Orbiter mission around a suitable to near earth asteroid coupled with flyby to one or more comets / asteroids Possible time frame : 2015

  22. Asteroid Mission: Science Goals & Mission Priorities Scientific objectives  Understanding Evolution of Asteroids  Shape, Size, Mass and Composition of Asteroids  Asteroids (e.g. Vesta and Ceres) as parent bodies of meteorites (differentiated and stony type)  Role of water/ice in controlling asteroid evolution  Thermal history, differentiation and core size Understanding the very early processes operating in Planetesimals and hence in Planets

  23. Hydrogen Envelope ION TAIL DUST TAIL COMA NUCLEUS COMET ORBIT SUN Target: Comet • Surface and Interior of Comet Nucleus • Composition of dust and gas in the coma • Details of thermal balance and outflow (sublimation of Ice) • Solar radiations & solar wind interaction • Samples of Comet Dust for Laboratory Studies Comet mission configuration to be based on the outcome of other such missions

  24. Mission to Mars • Orbiter mission to Mars to study Mars atmosphere, weather and solar wind-Mars interactions. • Instruments to be developed are for studying weak magnetic field and plasma • Timeframe : 2019

  25. Thank You

More Related