Competence Building in Complex Systems in the Developing Countries: the Case of Satellite Building in India
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Indian Satellite Navigation Programme
UUssee ooff EEqquuaattoorriiaall oorrbbiitt ffoorr IInnddiiaann SSaatteelllliittee NNaavviiggaattiioonn PPrrooggrraammmmee Presentation by D. Radhakrishnan ISRO HQ, India COSPAR & IAF Workshop, 44th Session of S&T, 13th February 2007 INDIAN SPACE PROGRAMME - Achievements TODAY, 2007 Applications driven programme Self reliance in building & launching satellites ONE AMONG E November 21, 1963 L C I 22 THE H LV Missions E SIX V H NATIONS C N PSLV GSLV U 10 4 A A L GSAT-3 4466 P ++ 66 SS//CC MMiissssiioonnss 20.9.04 P L E INSAT-3A GSAT-2 I C T 10.04.03 08.05.03 I KALPANA-1 A L T L INSAT-2E INSAT- 4A 12.09.02 I E 03.04.99 22.12.05 O T N A INSAT-3E S S CARTOSAT-2 ARYABHATA 28.09.03 INSAT-3B INSAT-3C 10.01.07 19.04.75 22.03.00 24.01.02 IRS-P5 IRS-1C 05.05.05 28.12.95 IRS-P3 IRS-P6 21.03.96 TES IRS-P4 17.10.03 IRS-1D 26.05.99 22.10.01 29.09.97 GGGAAAGGGAAANNN IIIRRRNNNSSSSSS Indian Regional Navigational Space Based Augmentation System Satellite System GGlloobbaall NNaavviiggaattiioonn SSaatteelllliittee SSyysstteemm ((GGNNSSSS)) Core Constellations S S P P G GPS – USA G GLONASS – Russia S S S S A A GALIELO - European Union N N O O L L G Augmentation Systems G • Ground Based Augmentation System (GBAS) o o e e l l i i l l a • Aircraft Based Augmentation Systems (ABAS) a G G • Space Based Augmentation System (SBAS) GGAAGGAANN ((GGPPSS AAnndd GGEEOO AAuuggmmeenntteedd SSaatteelllliittee NNaavviiggaattiioonn)) Objective Satellite Based Augmentation System To provide for -- • Satellite-based Communication, Navigation, Surveillance • Air Traffic Management -
Overview of Sensors for Applications
OVERVIEW OF SENSORS FOR APPLICATIONS Deepak Putrevu Head, MTDD/AMHTDG EM SPECTRUM Visible 0.4-0.7μm Near infrared (NIR) 0.7-1.5μm Optical Infrared Shortwave infrared (SWIR) 1.5-3.0μm Mid-wave infrared (MWIR) 3.0-8.0μm (OIR) Region Longwave IR(LWIR)/Thermal IR(TIR) 8.0-15μm Far infrared (FIR) Beyond15μm Gamma Rays X Rays UV Visible NIR SWIR Thermal IR Microwave P-band: ~0.25 – 1 GHz Microwave Region L-band: 1 -2 GHz S-band: 2-4 GHz •Sensors are 24x365 C-band: 4-8 GHz •Signal data characteristics X-band: 8-12 GHz unique to the microwave region of the EM spectrum Ku-band: 12-18 GHz K-band: 18-26 GHz •Response is primarily governed by geometric Ka-band: 26-40 GHz structures and hence V-band: 40 - 75 GHz complementary to optical W-band: 75-110 GHz imaging mm-wave: 110 – 300GHz Basic Interactions between Electromagnetic Energy and the Earth’s Surface Incident Power reflected, ρP Reflectivity: The fractional part of the radiation, P incident radiation that is reflected by the surface. Power absorbed, αP Absorptivity: the fractional part of the = Power emitted, εP incident radiation that is absorbed by the surface. Power transmitted, τP Emissivity: The ratio of the observed flux emitted by a body or surface to that of a P= Pr + Pt + Pa blackbody under the same condition. 푃 푃 푃 푟 + 푡 + 푎 = 1 푃 푃 푃 Transmissivity: The fractional part of the ρ + τ + α =1 radiation transmitted through the medium. At thermal equilibrium, absorption and emission are the same. -
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. -
History of the Indian Remote Sensing Programme
History of the Indian Remote Sensing Programme Ranganath Navalgund Vikram Sarabhai Distinguished Professor Indian Space Research Organisation Bangalore, India Workshop on Small Satellites & Sensor Technology for Disaster Management, Indo-US S&T Forum CANEUSMarch SSTDM 31, 2014 2014 BEGINNING Stared with the pioneering experiment of detecting Coconut Root Wilt Disease using Color Infrared Film in 1970s by Prof. P. R. Pisharoty. Jun 07,1979 Bhaskara-I (1979) and Bhaskara-II (1981) – Experimental Remote Sensing Satellites provided the Aerial view of Grove Area foundation for the operational Indian Remote Sensing Programme. Nov 20, 1981 (Coconut Root Wilt Disease Study) The Result is operational Indian Remote Sensing Programme with the launch of IRS-1A on March 17, 1988 CANEUS SSTDM 2014 DURING 1980s NRSA established Earth Station Complex at Annaram Village, Shadnagar, 59 km from Balanagar in 1979 to receive Landsat Data TERMINAL-1 (10M DIA) L & S Band 15 Mbps 1980-83: Landsat 2,3 & NOAA- 2, 3 1983-88: Landsat 5, ERS, SPOT & NOAA Today: Multimission ScenarioCANEUS - 4 SSTDMTerminals 2014 (7.5m) - upto 960Mbps EVOLUTION OF (Microwave RISAT-1 (2012) Capability) INDIAN EO SYSTEMS C Band SAR (5.35 GHz) IMS-1 (2008) (Hyperspectral HySI Sensor (64 bands, 506 m) Capability) TWSAT-MX (4 bands, 37 m) TES, Cartosat-1, 2/2A/2B (1999, (High Spatial Resolution 2005, 2007, 2008, 2010) & Stereo Capability) PAN : 2.5 m, 1m Fore +26o Aft: -5o Resourcesat-1/2 (2003, 2011) (Multi resolution, Frequent LISS-3: 23 m, 4 XS, observations, Better LISS-4: 5.8 -
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. -
Indian Remote Sensing Missions
ACKNOWLEDGEMENT This book, “Indian Remote Sensing Missions and Payloads - A Glance” is an attempt to provide in one place the information about all Indian Remote Sensing and scientific missions from Aryabhata to RISAT-1 including some of the satellites that are in the realization phase. This document is compiled by IRS Program Management Engineers from the data available at various sources viz., configuration data books, and other archives. These missions are culmination of the efforts put by all scientists, Engineers, and supporting staff across various centres of ISRO. All their works are duly acknowledged Indian Remote Sensing Missions & Payloads A Glance IRS Programme Management Office Prepared By P. Murugan P.V.Ganesh PRKV Raghavamma Reviewed By C.A.Prabhakar D.L.Shirolikar Approved By Dr.M. Annadurai Program Director, IRS & SSS ISRO Satellite Centre Indian Space Research Organisation Bangalore – 560 017 Table of Contents Sl.No Chapter Name Page No Introduction 1 1 Aryabhata 1.1 2 Bhaskara 1 , 2 2.1 3. Rohini Satellites 3.1 4 IRS 1A & 1B 4.1 5 IRS-1E 5.1 6 IRS-P2 6.1 7 IRS-P3 7.1 8 IRS 1C & 1D 8.1 9 IRS-P4 (Oceansat-1) 9.1 10 Technology Experiment Satellite (TES) 10.1 11 IRS-P6 (ResourceSat-1) 11.1 12 IRS-P5 (Cartosat-1) 12.1 13 Cartosat 2,2A,2B 13.1 14 IMS-1(TWSAT) 14.1 15 Chandrayaan-1 15.1 16 Oceansat-2 16.1 17 Resourcesat-2 17.1 18 Youthsat 18.1 19 Megha-Tropiques 19.1 20 RISAT-1 20.1 Glossary References INTRODUCTION The Indian Space Research Organisation (ISRO) planned a long term Satellite Remote Sensing programme in seventies, and started related activities like conducting field & aerial surveys, design of various types of sensors for aircraft surveys and development of number of application/utilization approaches. -
The Aryabhata Project
THE ARYABHATA PROJECT Edited by U. R, RAO, K. KASTURIRANGAN - ! - .’ j: ||)| if ijj} ' ' fpfjf- INDIAN ACADEMY OF SCIENCES Bangalore 660 006 Digitized by the Internet Archive in 2018 with funding from Public.Resource.Org https://archive.org/details/aryabhataprojectOOunse THE ARYABHATA PROJECT Edited by U. R. RAO, K. KASTURIRANGAN ISRO Satellite Centre, Bangalore INDIAN ACADEMY OF SCIENCES Bangalore 560 006 © 1979 by the Indian Academy of Sciences Reprinted from the Proceedings of the Indian Academy of Sciences, Section C: Engineering Sciences, Volume 1, pp. 117-343, 1978 Edited by U R Rao, K Kasturirangan and printed for the Indian Academy of Sciences by Macmillan India Press, Madras 600 002, India Foreword Space exploration and space travel have been the dream of mankind since early ages. When the first sputnik was launched into space in 1957 by USSR, the entire world was dramatically ushered into the space age. With the remarkable develop¬ ments that have taken place in space sciences and technology during the last two decades, some of mankind’s wildest dreams and visions—such as men walking on the moon, close-up pictures of Venus, Mars and Jupiter, in-situ exploration of planets, space docking near earth, space shuttle transportation—have all come true. The space era has opened up new windows into the skies, enabling scientists to obtain a view of the universe in X-rays and in ultraviolet, infrared and gamma rays, which had been inaccessible earlier. Developments in space technology now offer unique plat¬ forms to carry out remote sensing of our natural resources and unearth new ones in agriculture, forestry, mineralogy, hydrology, oceanography, geography and even cartography. -
India's Early Satellites – Spin-Stabilized and Bias Momentum
India’s Early Satellites – Spin-Stabilized and Bias Momentum ISRO Aryabhata – for Space Science (Launch date 19 April 1975) Aryabhata was India's first satellite It was launched by the Soviet Union from Kapustin Yar Mission type Astrophysics Satellite of Earth Aryabhata was built by the ISRO Launch date 19 April 1975 engineers to conduct Carrier rocket Cosmos-3M experiments related to X-ray astronomy, solar physics, and Mass 360.0 kg Power 46 W from solar panels aeronomy. Orbital elements Regime LEO The satellite reentered the Inclination 50.7º Orbital period 96 minutes Earth's atmosphere on 11 Apoapsis 619 km February 1992. Periapsis 563 km *National Space Science Data Center, NASA Goddard Space Flight Center Bhaskara (Earth Observation) Satellites (launched in 1979-1981)* Bhaskara-I and II Satellites were built by the ISRO, and they were India's first low orbit Earth Observation Satellite.They collected data on telemetry, oceanography, hydrology. Bhaskara-I, weighing 444 kg at launch, was launched on June 7, 1979 from Kapustin Yar aboard the Intercosmos launch vehicle. It was placed in an orbital Perigee of 394 km and Apogee of 399 km at an inclination of 50.7°. The satellite consisted of- Two television cameras operating in visible (0.6 micrometre) and near-infrared (0.8 micrometre) and collected data related to hydrology, forestry and geology. Satellite microwave radiometer (SAMIR) operating at 19 GHz and 22 GHz for study of ocean-state, water vapor, liquid water content in the atmosphere, etc. The satellite provided ocean and land surface data. Housekeeping telemetry was received until re-entry on 17 February 1989. -
PT-365-Science-And-Tech-2020.Pdf
SCIENCE AND TECHNOLOGY Table of Contents 1. BIOTECHNOLOGY ___________________ 3 3.11. RFID ___________________________ 29 1.1. DNA Technology (Use & Application) 3.12. Miscellaneous ___________________ 29 Regulation Bill ________________________ 3 4. DEFENCE TECHNOLOGY _____________ 32 1.2. National Guidelines for Gene Therapy __ 3 4.1. Missiles _________________________ 32 1.3. MANAV: Human Atlas Initiative _______ 5 4.2. Submarine and Ships _______________ 33 1.4. Genome India Project _______________ 6 4.3. Aircrafts and Helicopters ____________ 34 1.5. GM Crops _________________________ 6 4.4. Other weapons system _____________ 35 1.5.1. Golden Rice ________________________ 7 4.5. Space Weaponisation ______________ 36 2. SPACE TECHNOLOGY ________________ 8 4.6. Drone Regulation __________________ 37 2.1. ISRO _____________________________ 8 2.1.1. Gaganyaan _________________________ 8 4.7. Other important news ______________ 38 2.1.2. Chandrayaan 2 _____________________ 9 2.1.3. Geotail ___________________________ 10 5. HEALTH _________________________ 39 2.1.4. NaVIC ____________________________ 11 5.1. Viral diseases _____________________ 39 2.1.5. GSAT-30 __________________________ 12 5.1.1. Polio _____________________________ 39 2.1.6. GEMINI __________________________ 12 5.1.2. New HIV Subtype Found by Genetic 2.1.7. Indian Data Relay Satellite System (IDRSS) Sequencing _____________________________ 40 ______________________________________ 13 5.1.3. Other viral Diseases _________________ 40 2.1.8. Cartosat-3 ________________________ 13 2.1.9. RISAT-2BR1 _______________________ 14 5.2. Bacterial Diseases _________________ 40 2.1.10. Newspace India ___________________ 14 5.2.1. Tuberculosis _______________________ 40 2.1.11. Other ISRO Missions _______________ 14 5.2.1.1. Global Fund for AIDS, TB and Malaria42 5.2.2. -
NISAR Science Workshop – 2014
Science Workshop – 2014 NISAR Space Applications Centre NISAR Mission Overview Tapan Misra (ISRO) & Paul Rosen (JPL) Space Applications Centre (SAC) NASA ISRO Synthetic Aperture Radar (NISAR) NISAR Mission Overview Payload / Mission Characteristics Would Enable 1 L-band (24 cm wavelength) Low temporal decorrelation and foliage penetration 2 S-band (12 cm wavelength) Sensitivity to light vegetation 3 SweepSAR technique with Imaging Swath > Global data collection 240 km 4 Polarimetry (Single/Dual/Quad) Surface characterization and biomass estimation 5 12-day exact repeat Rapid Sampling 6 3 – 10 meters mode-dependent SAR resolution Small-scale observations 7 3 years science operations (5 years Time-series analysis consumables) 8 Pointing control < 273 arcseconds Deformation interferometry 9 Orbit control < 500 meters Deformation interferometry 10 > 30% observation duty cycle Complete land/ice coverage 11 Left/Right pointing capability Polar coverage, north and south th th *Mission Concept – Pre-decisional – for Planning and NISAR Science Workshop, SAC Ahmedabad – 17 & 18 Nov. 2014 2 Discussion Purposes Only Key Capabilities for NISAR Repeatable orbits and instrument pointing Swath width sufficient to cover ground-track spacing at equator Polarimetric synthetic aperture radar with “industry-standard” performance parameters valid over the full swath All imaging with the instrument boresight pointed 37 degrees off-nadir and +/- 90 degrees off the body-fixed velocity vector Orbit reconstruction to cm-scale accuracy for efficient interferometric processing and calibration Sufficient duty cycle and mission resources to strobe Earth’s land and ice on ascending and descending orbits each repeat cycle 24-hour turnaround on urgent retargeting and 5-hour latency for data designated as urgent th th *Mission Concept – Pre-decisional – for Planning and NISAR Science Workshop, SAC Ahmedabad – 17 & 18 Nov. -
Unmanned Satellites on Postage Stamps 42. Aryabhata, Bhaskara, Rohini, and Badr Series Satellites by Don Hillger - SU 5200 and Garry Toth (Coauthor)
Unmanned Satellites on Postage Stamps 42. Aryabhata, Bhaskara, Rohini, and Badr Series Satellites by Don Hillger - SU 5200 and Garry Toth (Coauthor) This is the forty-second in a series of quasi-spherical polyhedron, about 1.6 articles about unmanned satellites on m in diameter. postage stamps. In this article we cover Since the body of the spacecraft scientific satellites from Southern Asia: is similar for both Aryabhata and the Aryabhata, Bhaskara, and Rohini Bhaskara, it is assumed that the satellites from India, and the Badr antennas can be used to distinguish satellite from Pakistan. between the two. For Aryabhata, the TheAryabhata satellite was India’s antennas appear to be attached to the first satellite, launched 19 April 1975. widest part of the spacecraft body. For It was completely designed and Bhaskara, the antennas appear to be manufactured in India but launched by attached to the angled part of the body. Russia. The spacecraft, named after the The first Rohini was the first Indian- famous Indian astronomer Aryabhata built satellite that was also launched (476-550), was a scientific satellite by them, on 18 July 1980. Three used to measure cosmic X-rays, solar Rohinis were launched through 1983. neutrons, gamma rays, ionospheric Although some sources identify electrons, and UV rays. With 26 sides, it as a spherical satellite, 0.6 m in the spacecraft was quasi-spherical. diameter, the lone postal item from It appears on several stamps or other India featuring Rohini shows it as a postal items from India and Russia. polyhedron, similar to Aryabhata and Dominica is the only other country Bhaskara, but with one flattened end. -
Indian Remote Sensing Satellites (IRS)
Topic: Indian Remote Sensing Satellites (IRS) Course: Remote Sensing and GIS (CC-11) M.A. Geography (Sem.-3) By Dr. Md. Nazim Professor, Department of Geography Patna College, Patna University Lecture-5 Concept: India's remote sensing program was developed with the idea of applying space technologies for the benefit of human kind and the development of the country. The program involved the development of three principal capabilities. The first was to design, build and launch satellites to a sun synchronous orbit. The second was to establish and operate ground stations for spacecraft control, data transfer along with data processing and archival. The third was to use the data obtained for various applications on the ground. India demonstrated the ability of remote sensing for societal application by detecting coconut root-wilt disease from a helicopter mounted multispectral camera in 1970. This was followed by flying two experimental satellites, Bhaskara-1 in 1979 and Bhaskara-2 in 1981. These satellites carried optical and microwave payloads. India's remote sensing programme under the Indian Space Research Organization (ISRO) started off in 1988 with the IRS-1A, the first of the series of indigenous state-of-art operating remote sensing satellites, which was successfully launched into a polar sun-synchronous orbit on March 17, 1988 from the Soviet Cosmodrome at Baikonur. It has sensors like LISS-I which had a spatial resolution of 72.5 meters with a swath of 148 km on ground. LISS-II had two separate imaging sensors, LISS-II A and LISS-II B, with spatial resolution of 36.25 meters each and mounted on the spacecraft in such a way to provide a composite swath of 146.98 km on ground.