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DEPARTMENT of SPACE DEMAND NO.89 Department of Space A
Notes on Demands for Grants, 2005-2006 193 DEPARTMENT OF SPACE DEMAND NO.89 Department of Space A. The Budget allocations, net of recoveries, are given below: (In crores of Rupees) Budget 2004-2005 Revised 2004-2005 Budget 2005-2006 Major Head Plan Non-Plan Total Plan Non-Plan Total Plan Non-Plan Total Revenue 1836.01 331.29 2167.30 1661.10 340.00 2001.10 2192.16 348.00 2540.16 Capital 563.99 ... 563.99 538.90 ... 538.90 607.84 ... 607.84 Total 2400.00 331.29 2731.29 2200.00 340.00 2540.00 2800.00 348.00 3148.00 1. Secretariat - Economic Services 3451 ... 4.27 4.27 ... 4.78 4.78 ... 4.50 4.50 Space Research Space Technology Launch Vehicle Technology 2. Geo -Synchronous Satellite Launch Vehicle 3402 36.78 ... 36.78 39.44 ... 39.44 17.95 ... 17.95 3. GSLV MK-III Development. 3402 164.00 ... 164.00 152.53 ... 152.53 218.54 ... 218.54 5402 326.00 ... 326.00 237.47 ... 237.47 231.46 ... 231.46 Total 490.00 ... 490.00 390.00 ... 390.00 450.00 ... 450.00 4. Cryogenic Upper Stage (CUS) 3402 9.92 ... 9.92 8.02 ... 8.02 1.67 ... 1.67 Project 5402 1.00 ... 1.00 1.23 ... 1.23 ... ... ... Total 10.92 ... 10.92 9.25 ... 9.25 1.67 ... 1.67 5. Polar Satellite Launch Vehicle - 3402 122.50 ... 122.50 122.50 ... 122.50 108.73 ... 108.73 Continuation Project 5402 ... ... ... ... ... ... 11.27 ... 11.27 Total 122.50 .. -
Mission/PDS Build Schedule
Mission/PDS Build Schedule Last updated 30 Oct 2017: Updated ExoMars Rover, BepiColom, Chandrayaan-2, Psyche launch dates. Updated New Horizons 2014 MU69 flyby. Updated Juno EOM. Extended active missions: Venus Climate Orbiter, Dawn, Voyager 1/2, Mars Orbiter Mission. Project Summary Extended past mission wrapping up archives: Rosetta. Changed MESSENGER, Cassini to "Past" missions. Added new missions: Hope Mars, Mars Orbiter Mission-2, Martian Moon eXplorer. Removed AIM (cancelled). a = Adoption of PDS4 release(s) PDS4 Release Version 1.7 1.8 1.9 1.10 1.11 V V V V V d = Distribution of PDS4 data Lead PDS PDS4 Release FY17 FY18 FY19 FY20 FY21 FY22 FY23 FY24 FY25 FY26 FY27 FY28 Other Nodes Status Mission Node Version Adopted 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 MAVEN ATM PPI,NAIF Active 4 1.1-1.5 d d d d d d d d d d MOI Sep 2014; Extended through Sep 2018 Mars Science Laboratory/MSL/Curiosity GEO ATM,CIS,PPI,NAIF Active 3 Extended through Sep 2018 Mars Reconnaissance Orbiter/MRO GEO ATM,CIS,NAIF Active 3 Extended through Sep 2018 Study: pre-Phase A (response to proposal request) Mars Exploration Rover/MER/Opportunity GEO ATM,CIS,NAIF Active 3 Extended through Sep 2018 Formulation: Phase A (mission and systems definition) Mars Odyssey GEO CIS,NAIF Active 3 Extended through Sep 2018 Formulation: Phase B (preliminary design) InSight GEO ATM,CIS,PPI,NAIF Future 4 1.4-1.5 (?) a a a a a a/d d d d d d d d d d Launch May 2018; Land Nov 2018 Implementation: Phase C (design) / D (build, test, -
Overview of Chandrayaan-1 PDS (Planetary Data System) Products
Chandrayaan-1 PDS Data Products Archival Generation and Browse By Ajay Kumar Prashar HRDPD/SIPG Chandrayaan-1 SAC Data Processing Team Contents • ISDA (ISRO Science Data Archive) Overview • PDS (Planetary Data System) Overview • Mission & instrument Overview • Archive Process • Data Products Definitions • Data Products Archive Generation • Archive Organization : Mission & Instrument level • Visualizations of PDS Data Products (Ch1PDSViewer/NASAVIEW/USGS-ISIS) • Chandrayaan-1 Browse Application ISDA – Overview Central repository for all scientific and engineering data returned by ISRO’s planetary missions Established at Indian Space Science Data Centre (ISSDC) Bangalore - in 2008. ISDA archives data sets from following missions: Chandrayaan-1 Mars Orbiter Mission Astrosat Chandrayaan-2 (Future) ISDA adopted PDS as archive standard for generating mission & instrument specific data sets for the scientific user community ISDA provides international collaboration with IPDA (International Planetary Data Alliance) PDS - Overview Well known Archive standard for all the NASA planetary missions in the scientific user community. Adopted by ESA, JAXA and other space agencies across globe. Features of PDS Self structured, documented & Peer Review Data Sets Long-term access and usability of data ISRO had also adopted PDS3 for following missions Chandrayaan-1 Mars Orbiter Mission. ISRO will adopt PDS4 for Chandrayaan-2 and continue PDS4 for future planetary missions. PDS Home Page (http://pds.nasa.gov) Mission & Instruments – Overview Chandrayaan-1, India’s first mission to Moon, was launched successfully on 22 October 2008 from SDSC SHAR, Sriharikota. Spacecraft was orbiting around Moon at a height of 100 km from the lunar surface for chemical, mineralogical and photo-geologic mapping of the Moon. Spacecraft carried 11 scientific instruments built in India, USA, UK,Germany, Sweden and Bulgaria. -
G. Madhavan Nair - Wikipedia, the Free Encyclopedia
G. Madhavan Nair - Wikipedia, the free encyclopedia G. Madhavan Nair From Wikipedia, the free encyclopedia G. Madhavan Nair (Malayalam: ജി. മാധവ നായ) (born October 31, 1943) is the G Madhavan Nair present Chairman of Indian Space Research Organisation and Secretary to the Department of Space, Government of India since September 2003. He is also the Chairman, Space Commission and acts as the Chairman of Governing Body of the Antrix Corporation, Bangalore. Madhavan Nair was awarded the Padma Vibhushan, India's second highest civilian honour, on January 26, 2009.[1][2] Contents 1 Early life 2 Career 3 As Chairman of ISRO 4 Additional responsibilities G Madhavan Nair 5 Awards Born 31 October 1943 6 Honours Thiruvanathapuram, India 7 Fellowships/Memberships 8 Lashkar Threat Residence India 9 References Nationality Indian 10 External links Fields Rocket Technology Institutions Indian Space Research Organisation Bhabha Atomic Research Center Early life Alma mate r B.Sc. (Engineering - Electrical & Communication) (1966), College of Nair was born at Neyyattinkara near Thiruvananthapuram, Kerala, India. He also studied in his Engineering, Trivandrum early life in Kanyakumari District. He graduated with a B.Sc. in Engineering (1966) from College Known for Indian Space Program of Engineering, Thiruvananthapuram, Kerala University with specialization in Electrical & Communication Engineering. After his graduation Nair attended a training program at the Bhabha Notable Padma Bhushan (1998) awards Atomic Research Center (BARC) Training School, Mumbai. Padma Vibhushan (2009) Career Nair is a leading technologist in the field of rocket systems and has made significant contribution to the development of multi-stage satellite launch vehicles, achieving self-reliance in independent access to space using indigenous technologies. -
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. -
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 -
To the Moon and Beyond! Article
3/12/2020 Achieve3000: Lesson Printed by: Jessica Christian Printed on: March 12, 2020 To the Moon and Beyond! Article PART 1 NEW DELHI, India. Both India and China are moving ahead in space exploration. Both countries launched space missions in 2013. India's Mars Orbiter Mission (MOM) was sent to Mars in November. China's Chang'e 3 spaceship blasted off on its way to the moon in December. India India launched its first spacecraft bound for Mars on November 5, 2013. The craft spent almost a month in Earth's orbit. Then, on November 30, 2013, the orbiter went on its way to the Red Planet. "The Earth orbiting phase of the spacecraft ended. The spacecraft is now on a course to reach Mars after a journey of about 10 months around the sun," the Indian Space Research Organisation (ISRO) said in early December. The 3,000-pound (1,350-kilogram) orbiter is called Mangalyaan. That means "Mars craft" in Hindi. It must travel 485 million miles (780 million Photo credit and all related images: kilometers) to reach an orbit around Mars. It will take about 300 days. It is Arun Sankar K/AP expected to do this by September 2014. This is the Satish Dhawan Space Center in southern India. India sent its first spaceship to Mars in The orbiter will gather images and data. They will help in determining how November 2013. Martian weather systems work. India is also looking to MOM to figure out what happened to the large quantities of water that are believed to have once existed on Mars. -
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. -
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.