Recent Indian Space Missions - Update As on Feb 2016
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Ariane-5 Completes Flawless Third Test Flight
r bulletin 96 — november 1998 Ariane-5 Completes Flawless Third Test Flight A launch-readiness review conducted on Friday engine shut down and Maqsat-3 was 16 and Monday 19 October had given the go- successfully injected into GTO. The orbital ahead for the final countdown for a launch just parameters at that point were: two days later within a 90-minute launch Perigee: 1027 km, compared with the window between 13:00 to 14:30 Kourou time. 1028 ± 3 km predicted The launcher’s roll-out from the Final Assembly Apogee: 35 863 km, compared with the Building to the Launch Zone was therefore 35 898 ± 200 km predicted scheduled for Tuesday 20 October at 09:30 Inclination: 6.999 deg, compared with the Kourou time. 6.998 ± 0.05 deg predicted. On 21 October, Europe reconfirmed its lead in providing space Speaking in Kourou immediately after the flight, transportation systems for the 21st Century. Ariane-5, on its third Fredrik Engström, ESA’s Director of Launchers qualification flight, left no doubts as to its ability to deliver payloads and the Ariane-503 Flight Director, confirmed reliably and accurately to Geostationary Transfer Orbit (GTO). The new that: “The third Ariane-5 flight has been a heavy-lift launcher lifted off in glorious sunshine from the Guiana complete success. It qualifies Europe’s new Space Centre, Europe’s spaceport in Kourou, French Guiana, at heavy-lift launcher and vindicates the 13:37:21 local time (16:37:21 UT). technological options chosen by the European Space Agency.” This third Ariane-5 test flight was intended ESA’s Director -
CASTOR: a Wide-Field, UV Space Telescope
Astro2020 Activities and Projects White Paper CASTOR: A Wide-Field, UV Space Telescope Thematic Areas: Space Missions Ground-Based Activities and Projects Computation Astrophysics Theoretical Astrophysics Laboratory Astrophysics Principal Author: Peter L. Capak Name: Peter L. Capak Institution: Infrared Processing and Analysis Center, California Institute of Technology, 1200 E. California Blvd, Pasadena, CA, 91125, USA Email: [email protected] Phone: (626) 395-6422 Co-authors: Michael L. Balogh (University of Waterloo), Jessie L. Christiansen (NASA Exo- planet Science Institute, Caltech), Patrick Cotˆ e´ (National Research Council of Canada), Olivier Dore´ (Caltech, JPL), Maria Drout (University of Toronto), Christopher J. Evans (UK Astronomy Technology Centre, Royal Observatory Edinburgh), Andreas L. Faisst (IPAC, Caltech), Sarah C. Gallagher (University of Western Ontario), Carl J. Grillmair (IPAC, Caltech), Paul Harrison (Magellan Aerospace), John B. Hutchings (National Research Council of Canada), JJ Kavelaars (National Research Council of Canada), J.-F. Lavigne (ABB), Janice C. Lee (IPAC, Caltech), Shouleh Nikzad (Jet Propulsion Laboratory, California Institute of Technology), Jason D. Rhodes (Jet Propulsion Laboratory, California Institute of Technology), Jason F. Rowe (Bishop’s Univer- sity), Ruben´ Sanchez-Janssen (UK Astronomy Technology Centre, Royal Observatory Edinburgh), Alan D. Scott (Honeywell Aerospace), Charles Shapiro (Jet Propulsion Laboratory, California In- stitute of Technology), Melanie Simet (University of California Riverside), Harry I. Teplitz (IPAC, Caltech), Kim A. Venn (University of Victoria), Ludovic Van Waerbeke (University of British Columbia) 1 Abstract: CASTOR (The Cosmological Advanced Survey Telescope for Optical and UV Re- search) is a proposed Canadian-led mission that would provide high-resolution imaging and spec- troscopy in the UV/optical (0.15–0.55 µm) spectral region. -
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, -
A Quantitative Human Spacecraft Design Evaluation Model For
A QUANTITATIVE HUMAN SPACECRAFT DESIGN EVALUATION MODEL FOR ASSESSING CREW ACCOMMODATION AND UTILIZATION by CHRISTINE FANCHIANG B.S., Massachusetts Institute of Technology, 2007 M.S., University of Colorado Boulder, 2010 A thesis submitted to the Faculty of the Graduate School of the University of Colorado in partial fulfillment of the requirement for the degree of Doctor of Philosophy Department of Aerospace Engineering Sciences 2017 i This thesis entitled: A Quantitative Human Spacecraft Design Evaluation Model for Assessing Crew Accommodation and Utilization written by Christine Fanchiang has been approved for the Department of Aerospace Engineering Sciences Dr. David M. Klaus Dr. Jessica J. Marquez Dr. Nisar R. Ahmed Dr. Daniel J. Szafir Dr. Jennifer A. Mindock Dr. James A. Nabity Date: 13 March 2017 The final copy of this thesis has been examined by the signatories, and we find that both the content and the form meet acceptable presentation standards of scholarly work in the above mentioned discipline. ii Fanchiang, Christine (Ph.D., Aerospace Engineering Sciences) A Quantitative Human Spacecraft Design Evaluation Model for Assessing Crew Accommodation and Utilization Thesis directed by Professor David M. Klaus Crew performance, including both accommodation and utilization factors, is an integral part of every human spaceflight mission from commercial space tourism, to the demanding journey to Mars and beyond. Spacecraft were historically built by engineers and technologists trying to adapt the vehicle into cutting edge rocketry with the assumption that the astronauts could be trained and will adapt to the design. By and large, that is still the current state of the art. It is recognized, however, that poor human-machine design integration can lead to catastrophic and deadly mishaps. -
Precollimator for X-Ray Telescope (Stray-Light Baffle) Mindrum Precision, Inc Kurt Ponsor Mirror Tech/SBIR Workshop Wednesday, Nov 2017
Mindrum.com Precollimator for X-Ray Telescope (stray-light baffle) Mindrum Precision, Inc Kurt Ponsor Mirror Tech/SBIR Workshop Wednesday, Nov 2017 1 Overview Mindrum.com Precollimator •Past •Present •Future 2 Past Mindrum.com • Space X-Ray Telescopes (XRT) • Basic Structure • Effectiveness • Past Construction 3 Space X-Ray Telescopes Mindrum.com • XMM-Newton 1999 • Chandra 1999 • HETE-2 2000-07 • INTEGRAL 2002 4 ESA/NASA Space X-Ray Telescopes Mindrum.com • Swift 2004 • Suzaku 2005-2015 • AGILE 2007 • NuSTAR 2012 5 NASA/JPL/ASI/JAXA Space X-Ray Telescopes Mindrum.com • Astrosat 2015 • Hitomi (ASTRO-H) 2016-2016 • NICER (ISS) 2017 • HXMT/Insight 慧眼 2017 6 NASA/JPL/CNSA Space X-Ray Telescopes Mindrum.com NASA/JPL-Caltech Harrison, F.A. et al. (2013; ApJ, 770, 103) 7 doi:10.1088/0004-637X/770/2/103 Basic Structure XRT Mindrum.com Grazing Incidence 8 NASA/JPL-Caltech Basic Structure: NuSTAR Mirrors Mindrum.com 9 NASA/JPL-Caltech Basic Structure XRT Mindrum.com • XMM Newton XRT 10 ESA Basic Structure XRT Mindrum.com • XMM-Newton mirrors D. de Chambure, XMM Project (ESTEC)/ESA 11 Basic Structure XRT Mindrum.com • Thermal Precollimator on ROSAT 12 http://www.xray.mpe.mpg.de/ Basic Structure XRT Mindrum.com • AGILE Precollimator 13 http://agile.asdc.asi.it Basic Structure Mindrum.com • Spektr-RG 2018 14 MPE Basic Structure: Stray X-Rays Mindrum.com 15 NASA/JPL-Caltech Basic Structure: Grazing Mindrum.com 16 NASA X-Ray Effectiveness: Straylight Mindrum.com • Correct Reflection • Secondary Only • Backside Reflection • Primary Only 17 X-Ray Effectiveness Mindrum.com • The Crab Nebula by: ROSAT (1990) Chandra 18 S. -
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. -
6. the INTELSAT 17 Satellite
TWO COMMUNICATIONS SATELLITES READY FOR LAUNCH Arianespace will orbit two communications satellite on its fifth launch of the year: INTELSAT 17 for the international satellite operator Intelsat, and HYLAS 1 for the European operator Avanti Communications. The choice of Arianespace by leading space communications operators and manufacturers is clear international recognition of the company’s excellence in launch services. Based on its proven reliability and availability, Arianespace continues to confirm its position as the world’s benchmark launch system. Ariane 5 is the only commercial satellite launcher now on the market capable of simultaneously launching two payloads. Arianespace and Intelsat have built up a long-standing relationship based on mutual trust. Since 1983, Arianespace has launched 48 satellites for Intelsat. Positioned at 66 degrees East, INTELSAT 17 will deliver a wide range of communication services for Europe, the Middle East, Russia and Asia. Built by Space Systems/Loral of the United States, this powerful satellite will weigh 5,540 kg at launch. It will also enable Intelsat to expand its successful Asian video distrubution neighborhood. INTELSAT 17 will replace INTELSAT 702. HYLAS 1 is Avanti Communications’ first satellite. A new European satellite operator, Avanti Communications also chose Arianespace to orbit its HYLAS 2 satellite, scheduled for launch in the first half of 2012. HYLAS 1 was built by an industrial consortium formed by EADS Astrium and the Indian Space Research Organisation (ISRO), using a I-2K platform. Fitted with Ka-band and Ku-band transponders, the satellite will be positioned at 33.5 degrees West, and will be the first European satellite to offer high-speed broadband services across all of Europe. -
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. -
Ariane-DP GB VA209 ASTRA 2F & GSAT-10.Indd
A DUAL LAUNCH FOR DIRECT BROADCAST AND COMMUNICATIONS SERVICES Arianespace will orbit two satellites on its fifth Ariane 5 launch of the year: ASTRA 2F, which mainly provides direct-to-home (DTH) broadcast services for the Luxembourg-based operator SES, and the GSAT-10 communications satellite for the Indian Space Research Organization, ISRO. The choice of Arianespace by the world’s leading space communications operators and manufacturers is clear international recognition of the company’s excellence in launch services. Based on its proven reliability and availability, Arianespace continues to confirm its position as the world’s benchmark launch system. Ariane 5 is the only commercial satellite launcher now on the market capable of simultaneously launching two payloads and handling a complete range of missions, from launches of commercial satellites into geostationary orbit, to dedicated launches into special orbits. Arianespace and SES have developed an exceptional relationship of mutual trust over more than 20 years. ASTRA 2F will be the 36th satellite from the SES group (Euronext Paris and Luxembourg Bourse: SESG) to use an Ariane launcher. SES operates the leading direct-to-home (DTH) TV broadcast system in Europe, based on its Astra satellites, serving more than 135 million households via DTH and cable networks. Built by Astrium using a Eurostar E3000 platform, ASTRA 2F will weigh 6,000 kg at launch. Fitted with active Ku- and Ka-band transponders, ASTRA 2F will be positioned at 28.2 degrees East. It will deliver new-generation DTH TV broadcast services to Europe, the Middle East and Africa, and offers a design life of about 15 years. -
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 -
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 •