Isro Cal-Val Activities

Total Page:16

File Type:pdf, Size:1020Kb

Isro Cal-Val Activities ISRO CAL-VAL ACTIVITIES Dr.Ashok K.Shukla Head, Calibration & Validation Division Deputy Project Director, OCM2 CAL-VAL Team Leader, Saral/AltiKa CAL-VAL Space Applications Centre Indian Space Research Organisation Ahmedabad, India Outline • ISRO Cal-Val activities • OCM2 Ocean color Cal-Val • Kavaratti Cal-Val site in ocean • Vicarious calibration of OCM2 using Kavaratti • Briefs on other Cal-Val activities CAL/VAL activities for Land, Ocean & Atmosphere CAL-VAL OPTICAL MICROWAVE OCEANSAT RESOUR- INSAT-3D CARTOSAT OCM CESAT MEGHA- RISAT-1 OCEANSAT SARAL SAR SCATTERO- TROPIQUES METER ISRO missions Satellite Sensor(s) Satellite Sensor(s) IRS-1D LISS-III, PAN, WiFS RESOURCESAT-2 AWiFS, LISS-III, OCEANSAT-1 OCM LISS-IV TES TES PAN Youthsat LiVHySI KALPANA-1 DRT-S&R, VHRR RISAT-1 SAR INSAT-3A CCD camera, DRT- MEGHA- MADRAS, SAPHIR, S&R, VHRR TROPIQUES ScaRaB, ROSA CARTOSAT-1 PAN INSAT-3D Imager, Sounder CARTOSAT-2 PAN SARAL AltiKa, ARGOS IMS-1 HySI (IMS-1), MxT CARTOSAT-3 Panchromatic, VNIR, RISAT-2 SAR-X SWIR, LWIR OCEANSAT-2 OCM, ROSA, TES-HYS HySI Scatterometer OCEANSAT-3 OCM3 RESOURCESAT-3 AWIFS, LISS-III, Air-borne Sensor(s) LISS-IV DMSAR C-SAR RISAT-L SAR L AHySI Hyper-spectral Sr. Parameters Satellites Status Sr. Parameters Status 1 Integrated water vapor MT operational 34 Surface reflectance Research 2 Humidity profile MT operational 35 VI Research 3 Temperature profile MT operational 36 LAI Research 4 Wind speed MT operational 37 FAPAR Research 5 Precipitation MT operational 38 Insolation Research 6 SWR & LWR MT operational 39 Albedo Research 7 Cloud liquid water MT operational 40 LST Research 8 Wind speed SARAL/AltiKa operational 41 Net radiation Research 9 Significant wave height SARAL/AltiKa operational 42 Evapotranspiration Research 10 Sea surface height SARAL/AltiKa operational 43 Biomass Research 11 Chlorophyll-a, OCEANSAT-II operational 44 NPP Research 12 Total suspended matter OCEANSAT-II operational 45 Snow/Ice products Research 13 Kd (490nm) OCEANSAT-II operational 46 Climate change index Research 14 AOT(865nm) OCEANSAT-II operational 15 Wind speed OCEANSAT-II operational 16 Wind direction OCEANSAT-II operational 17 AMV (CMV,WVW) INSAT-3D operational 18 OLR INSAT-3D operational 19 UTH INSAT-3D operational 20 SST INSAT-3D operational 21 Aerosol, INSAT-3D operational Geo-physical 22 T, q – profile INSAT-3D operational 23 Stab. Indices INSAT-3D operational parameters/products 24 Fire, Smoke INSAT-3D operational 25 Fog INSAT-3D operational 26 Rain INSAT-3D operational 27 Snow cover INSAT-3D operational 28 NDVI INSAT-3D operational 29 Ozone INSAT-3D operational 30 Wind Speed RISAT operational 31 Oil slick map RISAT operational 32 vegetation extent map RISAT Research 33 Soil moisture RISAT Research OCM2 OCEAN COLOR CAL-VAL NPL, New Delhi PIs network for OCM-II Geo- SAC, Ahmedabad physical product validation IMMT,Bhubneshwar CIFE, Mumbai IITM, Pune NIO, Goa Andhra University; NIO- University NRSC, H’bad RC, Vizag NPOL, Cochin DST. Annamalai Kavaratti University INS Sagardhwani – Field experiments 25 N I N D I A 20 V i s a k h a p a t n a m Area 3 Area 2 Karwar 15 Area 1 10 K o c h i 5 N 65 E 70 75 80 85 90 95 E NPOL, Kochi Gujarat Department of Marine Satpati Sciences, Goa University Arnala Versova Revdanda Murud Shreevardhan Harnnai CIFE, Mumbai ARABIAN SEA N Vengurla National Institute of Oceanography, Visakhapatnam Vizag Offshore time-series Coastal time-series IMMT,Bhubaneswar ORISSA &WB COAST Centre for Advanced Study in Marine Biology, Annamalai University Site 1 (20, 30, 50, 100, 200m) Site 2 (20, 30, 50, 100, 200m) Site 3 (20, 30, 50, 100, 200m) Site 4 (20, 30, 50, 100, 200m) Site 5 (20, 30, 50, 100, 200m) Sagar Kanya transect during Dec.09 – Jan.10,2010 Lakshadweep The Autonomous Vertical Profiler with Chl sensor Chlorophyll (microgram / l) 0 0.5 1 1.5 2 2.5 3 0 Locations off Goa 5 10 15 Depth(m) 20 25 30 11:55 35 KAVARATTI CAL-VAL SITE FOR OCEAN COLOR Conceptualization of Kavaratti CAL–VAL site development ATMOS SENSOR AT KAVARATTI INSAT SOLAR PANELS/ CHL. DATA BATT. OPTICAL SENSOR DISPLAY SENSOR SAC PAIR OF OPTICAL DATA TRANS MET RECEIVING & MET BUOYS LOGGER MITTER SENSOR STATION GPS/MONI ARCHIVAL/ MOORING SENSOR RETRIEVAL SYSTEMS & ANALYSIS Kavaratti CAL-VAL site in deep ocean in Lakshadweep SITE SENSORS / CHARACTERI- BUOY DESIGN / PARAMETERS ZATION/FLUORO. MET.CALIBATION (SAC) CALIBRATION (NIOT) (NIO) DATA TRAN- LABORATORY SMISSION / ON ISLAND CAL-VAL RECEPTION (DST) SITE (SAC) DATA OPTICAL PRODUCTS CALIBRATION DATA DATA (SAC) (NPL) UTILIZATION ARCHIVAL (USERS) (MOSDAC) Location of Kavaratti Site N • Sea depth : 1900 mtrs. • Case-1 water • Low chlorophyll Kavaratti island Design of experiment for CAL-VAL Site characterization at Kavaratti using Saga-Sukti vessel DAY-1 : 25 Kms.x 25 Kms. DAY-2 : 10 Kms.x 10Kms. DAY-3 : 5 Kms.x 5 Kms. DAY-4 : 5 Kms.x 5 Kms. DAY-5 : 5 Kms.x 5Kms. DAY-6 : 5 Kms.x 5Kms. 125 PIXELS AGATTI 80 PIXELS - o o 72 22’E/10 42’N Station for data collection KAVARATTI OPTICAL & MET buoy deployment on Kavaratti site Kavaratti Optical buoy 20 January 2010 Seen by OCM2 New OPTICAL and MET buoys OPTICAL buoy Hyper- spectral radiometer OPTICAL Buoy drift on Kavaratti site INSAT 3C CAL-VAL site, Kavaratti Delhi Earth Station, New Delhi SAC/MOSDAC/INCOIS INSAT MSS TYPE-C System INSAT • One-way transmission S-BAND C-BAND HUB STATION INTERNET USERS (MSS TYPE-C TERMINALS) Data Transmission MSS Transmitter S – Band BPSK Synthesiz Modulator SSP er A • GPS acquisition • Data collection • Every hourly data Optical Respectiv Communicat transmission Radiomet e i-on GPS er\ Data Controller Receiver • Re-transmission to Sun Logger avoid data loss Photomet er •Transmission time : 0800-1700 hrs. Multiple 12V DC DC – DC DC Supply Supply Converter • Sleep /wakeup mode 9V – 36V To all feature Sub sys. Systems • Volume : 70kbytes/day Block Diagram of CAL – VAL Site Transmitter Data reception C-band 7.5m CAL/VAL Chain LNA&RF BPSK Interface FTP Down Demodulator Unit Server Converter (SHU) BPSK (1+1) FTP Demodulator Interface Server Unit Internet (SHU) • Error free packets from two transmissions • Data access through FTP server MOBY Vs OPTICAL BUOY Ship version of OPTICAL BUOY Spatial measurement CAL-VAL setup on Kavaratti island Instrument calibration CAL-VAL Sample analysis CIMEL Sun/sky Photometer on Kavaratti island 1020nm 870nm 670nm 440nm 500nm 380nm 0.2 AOD vs Time (30/11/2007) 0.18 0.16 0.14 0.12 0.1 AOD 0.08 0.06 0.04 0.02 0 2:13:38 2:31:11 2:38:02 2:49:52 2:58:25 Time (GMT) Parameters being measured at Kavaratti Sr. No. Instrument Parameters 1 Hyper spectral Spectral surface irradiance radiometer Spectral irradiance at 1.8m & 6.5m depth Spectral radiance at 2.26m & 7.2m depth Spectral attenuation coefficient for irradiance Spectral water leaving radiance Spectral normalized water leaving radiance Spectral remote sensing reflectance 2 Fluorometer Chlorophyll-a concentration Normalized turbidity unit 3 Met buoy sensors Air pressure Air temperature,Wind speed,Wind direction Relative humidity,Water temperature 4 Sun photometer Aerosol optical depth Integrated water vapor 5 Micro rain radar Rain rate 6 Disdrometer Rain intensity,Rain amount Total rain amount 7 Dr.Pisharoty Air pressure,Air temperature,Relative humidity sonde Wind speed,Wind direction Accuracy of in-situ parameters Sr.No. Instrument Parameter Measureme- nt error 1 In-air Hyper-spectral Down-welling irradiance +/- 2% radiometer (350-850nm) 2 In -water Hyper-spectral Up-welling radiance +/- 2% radiometer (350-850nm) Down-welling irradiance +/- 2% 3 Fluorometer Chlorophyll -a concentration 0 .02 g/ltr.* 4 Turbidity sensor Turbidity 0.1 NTU 5 Sun photometer Direct-sun irradiance +/- 2% Sky radiance +/- 2% 6 Anemometer Wind speed +/ - 2% Wind direction +/- 1% 7 Air temperature sensor Air temperature +/ - 0.1 oC 8 Hygrometer % Relative Humidity +/- 1% 9 Barometer Air pressure +/- 0.05% 10 Thermometer Sea surface temperature +/-0.005 oC Integrating sphere for Radiance calibration Calibration setup for irradiance calibration Absolute rad./wavelength calibration of radiometers Radiance calibration Wavelength calibration HR05144-Lu 35th - CEOS Working Group on Calibration and Validation 24-28, September, 2012, Hyderabad, India Temporal stability of radiometric sensor Power mode HR050145 Ed Sensor Power mode HR050145 Ed Sensor Power mode Current mode Peak RMS Median RMS Median Error Error Error Error UV (390-405nm) 0.3 0.3 0.2 0.2 Blue (440-470nm) 0.2 0.2 0.1 0.1 Green(500-610nm) 0.3 0.3 0.1 0.1 White(440-610nm) 0.3 0.3 0.1 0.1 Red(700-730nm) 0.6 0.6 0.1 -1.0 IR(800-830nm) 0.4 0.5 0.1 -0.1 Entire spectrum(390-830nm) 0.4 0.3 0.2 0.1 CAL-VAL Package for data archival/ retrieval Data dissemination and web portal DATA ANALYSIS FOR VICARIOUS CALIBRATION OF OCM2 Solar irradiance at sea surface (Good day at Kavaratti) (OCM bands) 1.4 412n 1.2 m 1 443n m 0.8 490n 0.6 m 510n 0.4 m 0.2 555n m Es ( uW/cm2/nm)Es 0 Time ( hrs.) OPTICAL buoy tilt during deployment nLw from OPTICAL buoy during deployment Rrs from OPTICAL buoy during deployment Vicarious calibration of OCM2 sensor Water-leaving radiance (in situ) Total ozone + Rayleigh radiance L Atmospheric P r Lr ()F' ()P (, ,)/ 4 r r0 r 0 r 0 pressure P0 + Whitecap correction Lwc Whitecap radiance & F0 cos0 diffuse transmission L 0.22* f *t( ,)* wc 0 t exp- / 2 / cos + r oz Aerosol radiance, L (single as AOD, SSA scattering approximation) (CIMEL inversion) Las F0a () a ()Pa (,0 ,)/ 4 cos + Top-of-the-atmosphere Top-of-the-atmosphere (in situ) (satellite) L (λ) + L (λ) + t(λ)L (λ) + t(λ)L (λ) r as w wc Vicarious gain 35th - CEOS Working Group on Calibration and Validation 24-28, September, 2012, Hyderabad, India Satellite radiance extraction 5x5 pixel (sub-set OCM2 band Geometric extraction) over Imagery data correction Matchup criteria observation point Yes Satellite radiance Matchup criteria for Vicarious calibration extraction In situ geo- location Select pixels with NGP within ±1.5*σ*mean Find the Yes Sensor zenith closest pixel < 60o and Solar zenith < 75o Is NGP > TNP/2+1 Yes Exclude flagged Yes Total no.
Recommended publications
  • Remote Sensing in India
    Remote Sensing in India India’s Remote Sensing starts following the successful demonstration flights of Bhaskara-1 and Bhaskara-2 satellites launched in 1979 and 1981, respectively, with the development of indigenous Indian Remote Sensing (IRS) satellite program. Indian Remote Sensing (IRS) satellite system was commissioned with the launch of IRS-1A, in 1988. With many satellites in operation, IRS is the largest civilian remote sensing satellite constellation in the world providing imageries in a variety of spatial resolutions, spectral bands and swaths. Data from Indian Remote Sensing satellites are used for various applications of resources survey and management under the National Natural Resources Management System (NNRMS in following: Pre harvest crop area and production estimation of major crops. Drought/irrigation monitoring and assessment based on vegetation condition. Flood risk zone mapping and flood damage assessment. Hydro-geomorphologic maps for locating underground water resources for drilling well. Snow-melt run-off estimates for planning water use in downstream projects. Land use and land cover mapping. Urban planning. Forest survey. Wetland mapping. Environmental impact analysis. Mineral Prospecting. Coastal studies. India’s Recent IRS satellites 2012: Radar Imaging Satellite-1 (RISAT-1) imaging of the surface features during both day and night under all weather conditions. 2011: Megha-Tropiques, for studying the water cycle and energy exchanges in the tropics. 2011: RESOURCESAT-2 to continue the remote sensing data services to global users provided by RESOURCESAT-1, and to provide data with enhanced multispectral and spatial coverage as well. 2010: Cartosat-2B to provide multiple spot scene imageries. It is capable of imaging a swath (geographical strip) of 9.6 km with a resolution of better than 1 metre.
    [Show full text]
  • Indian Payload Capabilities for Space Missions
    INDIAN PAYLOAD CAPABILITIES FOR 13, Bangalore - SPACE MISSIONS July 11 A.S. Kiran Kumar Director Space Applications Centre International ASTROD Symposium, Ahmedabad th 5 Application-specific EO payloads IMS-1(2008) RISAT-1 (2012) MX/ HySI-T C-band SAR CARTOSAT-2/2A/2B RESOURCESAT-2 (2011) (2007/2009/2010) LISS 3/ LISS 4/AWiFS PAN RESOURCESAT-1 (2003) LISS 3/ LISS 4 AWiFS CARTOSAT-1 (2005) (Operational) STEREOPAN Megha-Tropiques (2011) TES(2001) MADRAS/SAPHIR/ScARaB/ Step& Stare ROSA PAN OCEANSAT-2 (2009) OCM/ SCAT/ROSA YOUTHSAT(2011) LiV HySI/RaBIT INSAT-3A (2003) KALPANA-1 (2002) VHRR, CCD VHRR Application-specific EO payloads GISAT MXVNIR/SWIR/TIR/HySI RISAT-3 RESOURCESAT-3A/3B/3C L-band SAR CARTOSAT-3 RESOURCESAT-2A LISS 3/LISS 4/AWiFS PAN LISS3/LISS4/AWiFS RESOURCESAT-3 LISS 3/LISS 4/ CARTOSAT-2C/2D AWiFS (Planned) PAN RISAT-1R C-band SAR SARAL Altimeter/ARGOS OCEANSAT-3 OCM , TIR GISAT MXVNIR/SWIR/ INSAT- 3D TIR/HySI Imager/Sounder EARTH OBSERVATION (LAND AND WATER) RESOURCESAT-1 IMS-1 RESOURCESAT-2 RISAT-1 RESOURCESAT-2A RESOURCESAT-3 RESOURCESAT-3A/3B/3C RISAT-3 GISAT RISAT-1R EARTH OBSERVATION (CARTOGRAPHY) TES CARTOSAT-1 CARTOSAT-2/2A/2B RISAT-1 CARTOSAT-2C/2D CARTOSAT-3 RISAT-3 RISAT-1R EARTH OBSERVATION (ATMOSPHERE & OCEAN) KALPANA-1 INSAT- 3A OCEANSAT-1 INSAT-3D OCEANSAT-2 YOUTHSAT GISAT MEGHA–TROPIQUES OCEANSAT-3 SARAL Current observation capabilities : Optical Payload Sensors in Spatial Res. Swath/ Radiometry Spectral bands Repetivity/ operation Coverage (km) revisit CCD 1 1 Km India & 10 bits 3 (B3, B4, B5) 4 times/ day surround.
    [Show full text]
  • Drafting Committee for the 'Asia‐Pacific
    Drafting Committee for the ‘Asia‐Pacific Plan of Action for Space Applications for Sustainable Development (2018‐2030) Dr Rajeev Jaiswal EOS Programme Office Indian Space Research Organisation (ISRO) India Bangkok, Thailand 31 May ‐ 1 June 2018 India’s Current Space Assets Communication Satellites • 15 Operational (INSAT- 4A, 4B, 4CR and GSAT- 6, 7, 8, 9 (SAS), 10, 12, 14, 15, 16, 17, 18 & 19) • >300 Transponders in C, Ext C & Ku bands Remote sensing Satellites • Three in Geostationary orbit (Kalpana-1, INSAT 3D & 3DR) • 14 in Sun-synchronous orbit (RESOURCESAT- 2 & 2A; CARTOSAT-1/ 2 Series (5); RISAT-2; OCEANSAT 2; MEGHA-TROPIQUES; SARAL, SCATSAT-1) Navigation Satellites : 7 (IRNSS 1A - IG) & GAGAN Payloads in GSAT 8, 10 & 15 Space Science: MOM & ASTROSAT 1 Space Applications Mechanism in India Promoting Space Technology Applications & Tools For Governance and Development NATIONAL MEET “There should not be any space between common man and space technology” . 160 Projects across 58 Ministries . Web & Mobile Applications : 200+ . MoUs with stakeholders : 120+ . Capacity Building : 10,000+ . Space Technology Cells : 21 17 STATE MEETS Haryana, Bihar, Uttarakhand, Mizoram, Nagaland, Rajasthan, Punjab, Jharkhand, Meghalaya, Himachal 20 58 Pradesh, Kerala, Chhattisgarh, Assam, Madhya Ministries Ministries Pradesh, Tamil Nadu, Mizoram & Uttar Pradesh Space Applications Verticals SOCIO ECONOMIC SECURITY SUSTAINABLE DEVELOPMENT Food Impact Assessment Water Bio- Resources Conservation Energy Fragile & Coastal Ecosystem Health Climate Change Induced
    [Show full text]
  • 25 Years of Indian Remote Sensing Satellite (IRS)
    2525 YearsYears ofof IndianIndian RemoteRemote SensingSensing SatelliteSatellite (IRS)(IRS) SeriesSeries Vinay K Dadhwal Director National Remote Sensing Centre (NRSC), ISRO Hyderabad, INDIA 50 th Session of Scientific & Technical Subcommittee of COPUOS, 11-22 Feb., 2013, Vienna The Beginning • 1962 : Indian National Committee on Space Research (INCOSPAR), at PRL, Ahmedabad • 1963 : First Sounding Rocket launch from Thumba (Nov 21, 1963) • 1967 : Experimental Satellite Communication Earth Station (ESCES) established at Ahmedabad • 1969 : Indian Space Research Organisation (ISRO) established (15 August) PrePre IRSIRS --1A1A SatellitesSatellites • ARYABHATTA, first Indian satellite launched in April 1975 • Ten satellites before IRS-1A (7 for EO; 2 Met) • 5 Procured & 5 SLV / ASLV launch SAMIR : 3 band MW Radiometer SROSS : Stretched Rohini Series Satellite IndianIndian RemoteRemote SensingSensing SatelliteSatellite (IRS)(IRS) –– 1A1A • First Operational EO Application satellite, built in India, launch USSR • Carried 4-band multispectral camera (3 nos), 72m & 36m resolution Satellite Launch: March 17, 1988 Baikanur Cosmodrome Kazakhstan SinceSince IRSIRS --1A1A • Established of operational EO activities for – EO data acquisition, processing & archival – Applications & institutionalization – Public services in resource & disaster management – PSLV Launch Program to support EO missions – International partnership, cooperation & global data sets EarlyEarly IRSIRS MultispectralMultispectral SensorsSensors • 1st Generation : IRS-1A, IRS-1B •
    [Show full text]
  • The Space-Based Global Observing System in 2010 (GOS-2010)
    WMO Space Programme SP-7 The Space-based Global Observing For more information, please contact: System in 2010 (GOS-2010) World Meteorological Organization 7 bis, avenue de la Paix – P.O. Box 2300 – CH 1211 Geneva 2 – Switzerland www.wmo.int WMO Space Programme Office Tel.: +41 (0) 22 730 85 19 – Fax: +41 (0) 22 730 84 74 E-mail: [email protected] Website: www.wmo.int/pages/prog/sat/ WMO-TD No. 1513 WMO Space Programme SP-7 The Space-based Global Observing System in 2010 (GOS-2010) WMO/TD-No. 1513 2010 © World Meteorological Organization, 2010 The right of publication in print, electronic and any other form and in any language is reserved by WMO. Short extracts from WMO publications may be reproduced without authorization, provided that the complete source is clearly indicated. Editorial correspondence and requests to publish, reproduce or translate these publication in part or in whole should be addressed to: Chairperson, Publications Board World Meteorological Organization (WMO) 7 bis, avenue de la Paix Tel.: +41 (0)22 730 84 03 P.O. Box No. 2300 Fax: +41 (0)22 730 80 40 CH-1211 Geneva 2, Switzerland E-mail: [email protected] FOREWORD The launching of the world's first artificial satellite on 4 October 1957 ushered a new era of unprecedented scientific and technological achievements. And it was indeed a fortunate coincidence that the ninth session of the WMO Executive Committee – known today as the WMO Executive Council (EC) – was in progress precisely at this moment, for the EC members were very quick to realize that satellite technology held the promise to expand the volume of meteorological data and to fill the notable gaps where land-based observations were not readily available.
    [Show full text]
  • Design of the Wavefront Sensor Unit of ARGOS, the LBT Laser Guide Star System
    UNIVERSITA` DEGLI STUDI DI FIRENZE Dipartimento di Fisica e Astronomia Scuola di Dottorato in Astronomia Ciclo XXIV - FIS05 Design of the wavefront sensor unit of ARGOS, the LBT laser guide star system Candidato: Marco Bonaglia arXiv:1203.5081v1 [astro-ph.IM] 22 Mar 2012 Tutore: Prof. Alberto Righini Cotutore: Dott. Simone Esposito A common use for a glass plate is as a beam splitter, tilted at an angle of 45◦ [:::] Since this can severely degrade the image, such plate beam splitters are not recommended in convergent or divergent beams. W. J. Smith, Modern Optical Engineering. Contents 1 Introduction 1 1.1 The Large Binocular Telescope . 2 1.2 LUCI . 4 1.3 First Light AO system . 5 1.3.1 Angular anisoplanatism . 8 1.4 Wide field AO correction . 9 1.5 Laser guide star AO . 10 1.5.1 Limits of LGS AO . 11 1.5.2 Rayleigh LGS . 13 1.6 LGS-GLAO facilities . 14 1.6.1 GLAS . 15 1.6.2 The MMT GLAO system . 15 1.6.3 SAM . 18 2 ARGOS: a laser guide star AO system for the LBT 21 2.1 System design . 22 2.2 Study of ARGOS performance . 29 2.2.1 The simulation code . 30 2.2.2 Results of ARGOS end-to-end simulations . 36 3 The wavefront sensor dichroic 43 3.1 Effects of a window in a convergent beam . 43 3.2 Aberration compensation with window shape . 47 3.2.1 Effects of a wedge between surfaces . 48 3.2.2 Effects of a cylindrical surface .
    [Show full text]
  • India and China Space Programs: from Genesis of Space Technologies to Major Space Programs and What That Means for the Internati
    University of Central Florida STARS Electronic Theses and Dissertations, 2004-2019 2009 India And China Space Programs: From Genesis Of Space Technologies To Major Space Programs And What That Means For The Internati Gaurav Bhola University of Central Florida Part of the Political Science Commons Find similar works at: https://stars.library.ucf.edu/etd University of Central Florida Libraries http://library.ucf.edu This Masters Thesis (Open Access) is brought to you for free and open access by STARS. It has been accepted for inclusion in Electronic Theses and Dissertations, 2004-2019 by an authorized administrator of STARS. For more information, please contact [email protected]. STARS Citation Bhola, Gaurav, "India And China Space Programs: From Genesis Of Space Technologies To Major Space Programs And What That Means For The Internati" (2009). Electronic Theses and Dissertations, 2004-2019. 4109. https://stars.library.ucf.edu/etd/4109 INDIA AND CHINA SPACE PROGRAMS: FROM GENESIS OF SPACE TECHNOLOGIES TO MAJOR SPACE PROGRAMS AND WHAT THAT MEANS FOR THE INTERNATIONAL COMMUNITY by GAURAV BHOLA B.S. University of Central Florida, 1998 A dissertation submitted in partial fulfillment of the requirements for the degree of Master of Arts in the Department of Political Science in the College of Arts and Humanities at the University of Central Florida Orlando, Florida Summer Term 2009 Major Professor: Roger Handberg © 2009 Gaurav Bhola ii ABSTRACT The Indian and Chinese space programs have evolved into technologically advanced vehicles of national prestige and international competition for developed nations. The programs continue to evolve with impetus that India and China will have the same space capabilities as the United States with in the coming years.
    [Show full text]
  • Glimpses of Indian Space Programme
    Presentation at the M. V. DHEKANE, International Symposium Associate Director (R&D) in Tokyo, on Vikram Sarabhai Space Centre, Stable use of Outer Space Indian Space Research Organisation 1 during March 3-4, 2016 Trivandrum, India “There are some who question the relevance of space activities in a developing nation. To us, there is no ambiguity of purpose. We are convinced that if we are to play a meaningful role in the comity of nations we should be second to none in the applications of advanced technologies to the real problems of man and Society.” Dr. Vikram A Sarabhai 2 The First Indian Rockets…. Rohini-75 (RH-75) The First rocket made by India and launched from Thumba 20-Nov-1967 Nike-Apache The First sounding rocket launched from Thumba 21-Nov-1963 3 Sounding Rockets 4 ISRO Launch vehicles SLV-3 to GSLV MkIII • GTO Mission • Cryogenics • Maraging Steel, Large Booster • Strap-on Technology • Liquid Propulsion • Closed loop Guidance • Gimbal Control, Flex Nozzle • Onboard RTD • Multiple Satellites injection • Bulbous Heat Shield • Vertical Integration • Solid propulsion • Inertial Systems • Open loop guidance • Orbital Mission GSLV Mk III • Heavy Cryogenics GSLV • Large solid & liquid (2000) Boosters 10000 4500 SLV-3 ASLV PSLV (1994) (1980) (1988) 3000 LEO PAYLOADS (KG) GSLV Mk III Launch Vehicle SLV ASLV PSLV GSLV (Under development) Lift-off weight 17 40 295 450 635 (Tonnes) Payload (kg) 40 (LEO) 150 (LEO) 1600 (SSO) 2000 (GTO) 4000 (GTO) 5 Indian Space programme VISION: Harness space technology for national development, while pursuing
    [Show full text]
  • Highlights in Space 2010
    International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no.
    [Show full text]
  • Annual Report 2017 - 2018 Annual Report 2017 - 2018 Citizens’ Charter of Department of Space
    GSAT-17 Satellites Images icro M sat ries Satellit Se e -2 at s to r a C 0 SAT-1 4 G 9 -C V L S P III-D1 -Mk LV GS INS -1 C Asia Satell uth ite o (G S S A T - 09 9 LV-F ) GS ries Sat Se ellit t-2 e sa to 8 r -C3 a LV C PS Annual Report 2017 - 2018 Annual Report 2017 - 2018 Citizens’ Charter of Department Of Space Department Of Space (DOS) has the primary responsibility of promoting the development of space science, technology and applications towards achieving self-reliance and facilitating in all round development of the nation. With this basic objective, DOS has evolved the following programmes: • Indian National Satellite (INSAT) programme for telecommunication, television broadcasting, meteorology, developmental education, societal applications such as telemedicine, tele-education, tele-advisories and similar such services • Indian Remote Sensing (IRS) satellite programme for the management of natural resources and various developmental projects across the country using space based imagery • Indigenous capability for the design and development of satellite and associated technologies for communications, navigation, remote sensing and space sciences • Design and development of launch vehicles for access to space and orbiting INSAT / GSAT, IRS and IRNSS satellites and space science missions • Research and development in space sciences and technologies as well as application programmes for national development The Department Of Space is committed to: • Carrying out research and development in satellite and launch vehicle technology with a goal to achieve total self reliance • Provide national space infrastructure for telecommunications and broadcasting needs of the country • Provide satellite services required for weather forecasting, monitoring, etc.
    [Show full text]
  • By Prof. Ram Gopal
    STATEMENT BY PROF. RAM GOPAL YADAV, MEMBER OF PARLIAMENT, ON AGENDA ITEM 51 – INTERNATIONAL COOPERATION IN THE PEACEFUL USERS OF OUTER SPACE IN THE GENERAL DEBATE OF THE SPECIAL POLITICAL AND DECOLONIZATION COMMITTEE [4TH COMMITTEE] OF THE 66TH SESSION OF THE UNITED NATIUONS GENERAL ASSEMBLY ON OCTOBER 13, 2011 Madam Chair The Indian Delegation is pleased to note the successful deliberations of the 54th session of UN-COPUOS, under the able chairmanship of Mr. Dumitru-Dorin Prunariu of Romania, and the substantial progress made during the session. The delegation notes with appreciation that UNCOPUOS, under the mandate of the General Assembly, continues to contribute significantly towards capacity building for sustainable development, and strengthening international co-operation to utilise outer space for peaceful purposes towards serving the humanity. The Indian Delegation also expresses its full satisfaction at the work carried out by the two sub-committees of UNCOPUOS, the Scientific and Technical Sub-committee at its 48th session and the Legal Sub- committee at its 50th session. Madam Chair While acknowledging the significant achievements of various member states in space endeavors during the last one year, the Indian delegation desires to brief the Assembly on the significant achievements made by India in the field of space since the last Session. On April 20, 2011, the Polar Satellite Launch Vehicle (PSLV C-16) precisely placed RESOURCESAT-2 and two auxiliary satellites namely YOUTHSAT and X-SAT into their intended orbits. RESOURCESAT-2 is augmenting the multispectral imaging capability of India as a follow-on mission to RESOURCESAT-1. YOUTHSAT is a small satellite built with participation of the Moscow State University; and X-SAT is a small satellite built by Nanyang Technological University (NTU) with ISRO’s support.
    [Show full text]
  • + Return to Flight Implementation Plan -- 12Th Edition (8.4 Mb PDF)
    NASA’s Implementation Plan for Space Shuttle Return to Flight and Beyond A periodically updated document demonstrating our progress toward safe return to flight and implementation of the Columbia Accident Investigation Board recommendations June 20, 2006 Volume 1, Twelfth Edition An electronic version of this implementation plan is available at www.nasa.gov NASA’s Implementation Plan for Space Shuttle Return to Flight and Beyond June 20, 2006 Twelfth Edition Change June 20, 2006 This 12th revision to NASA’s Implementation Plan for Space Shuttle Return to Flight and Beyond provides updates to three Columbia Accident Investigation Board Recommendations that were not fully closed by the Return to Flight Task Group, R3.2-1 External Tank (ET), R6.4-1 Thermal Protection System (TPS) On-Orbit Inspection and Repair, and R3.3-2 Orbiter Hardening and TPS Impact Tolerance. These updates reflect the latest status of work being done in preparation for the STS-121 mission. Following is a list of sections updated by this revision: Message from Dr. Michael Griffin Message from Mr. William Gerstenmaier Part 1 – NASA’s Response to the Columbia Accident Investigation Board’s Recommendations 3.2-1 External Tank Thermal Protection System Modifications (RTF) 3.3-2 Orbiter Hardening (RTF) 6.4-1 Thermal Protection System On-Orbit Inspect and Repair (RTF) Remove Pages Replace with Pages Cover (Feb 17, 2006) Cover (Jun. 20, 2006 ) Title page (Feb 17, 2006) Title page (Jun. 20, 2006) Message From Michael D. Griffin Message From Michael D. Griffin (Feb 17, 2006)
    [Show full text]