DOCSLIB.ORG

SICSA Mars Project

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
SICSA Mars Project SICSA Mars Project Space Architecture Spring 2010 Jessica Corbett James Doehring Frank Eichstadt Michael Fehlinger Kristine Ferrone Loi Nguyen Sasakawa International Center for Space Architecture, University of Houston College of Architecture Mission Statement: Student Project • Explore and define an architectural framework through which to study space architecture, space operations and mission planning, and functional relationships of systems, elements and people • Facilitate multi-disciplinary and cooperative study involving numerous students pursuing discrete aspects of the architecture Sasakawa International Center for Space Architecture, University of Houston College of Architecture Mission Statement: Mars Architecture • Provide sustainable, scalable and expandable capability to access and operate throughout the Martian system • Enable human visitation and Earth-return from Martian system, including orbits, natural satellites and eventually to the surface • Enable recovery of Martian artifacts • Contribute to the continued evolution Sasakawa International Center for Space Architecture, University of Houston College of Architecture Context of Mars Exploration Sasakawa International Center for Space Architecture, University of Houston College of Architecture Deployment Strategy • Earth Region – Incoming –Surface •Crew •Artifacts • Industry – Solar Orbit • Academia • Communication Satellites • Politics • Mars Region • Launch facilities – Approach –Orbital •Braking • LEO construction –Orbital • L4/L5 depot •OMV Ops • Departure trajectory • Depot • Interplanetary Region – Moons – Outgoing •OMV Ops •Crew •ISRU • Cargo Sasakawa International Center for Space Architecture, University of Houston College of Architecture Current Launch P/L Mass Launch Site Vehicle to LEO Ariene 5 Kourou, French Guiana 21 MT Atlas V KSC, Vandenberg AFB 20 MT Earth Surface Delta 4 Heavy KSC, Vandenberg AFB 25.8 MT H-II Tanegashima, Japan 19 MT • Manufacture all new components Proton M Baikonur, Kazahkstan 22 MT -Baikonur, Kazahkstan Soyuz FG/ST 7.8 MT • Acquire all existing components -Kourou, French Guiana -Baikonur, Kazakhstan • Assemble some components Zenit 3SL -Sea Launch Facility 5 MT (equator) • Tap into communications infrastructure Future Launch P/L Mass • Use various launch sites & vehicles Vehicle Launch Site to LEO Angara Vostochny, Russia 24.5 MT – All Components to LEO Falcon 9 Heavy KSC 32 MT GSLV Mark 3 Sriharikota Island, India 10 MT – Multiple launch options: Long March (CZ- NGLV) Hainan Island, China 25MT Taurus 2 Wallops Island, Virginia 5.5 MT Sasakawa International Center for Space Architecture, University of Houston College of Architecture Low Earth Orbit • Depot • Orbital Maneuvering –ISS Vehicle (OMV) – Fuel • Existing communication – Assembly/Repair/Refurb structure – Logistics • Crew Vehicle/Habitaxi • Earth re-entry Sasakawa International Center for Space Architecture, University of Houston College of Architecture LaGrangian Point 1, 4 or 5 •OMV • Depot – Staging – Fuel – Assembly/Repair/Refurb – Logistics • Crew Vehicle/Habitaxi Sasakawa International Center for Space Architecture, University of Houston College of Architecture Trans-Mars/Trans-Earth • Communication Satellites • Trans-Mars/Trans-Earth Vehicle – Propulsion System – Payload Spine – Propellant – Power System – Communication Components – Payload Elements Sasakawa International Center for Space Architecture, University of Houston College of Architecture Martian Moon Orbits • Robotics • Robotic Insitu Vehicle • ISRU option • Depot / Mars Observation Sasakawa International Center for Space Architecture, University of Houston College of Architecture Low Mars Orbit • Depot – Staging – Fuel – Assembly/Repair/Refurb – Logistics •OMV • Crew Vehicle/Habitaxi • Satellites – Communications – Navigation – Surveillance – Power beaming • Descent/Ascent Vehicle Sasakawa International Center for Space Architecture, University of Houston College of Architecture Mars Surface • Descent/Ascent Vehicle – Human – Cargo •ISRU • Robotics Capability • Communications/ Navigation • Surface Mobility • Habitation Modules • Surface Depot/Outpost • Environmental Robustitude Sasakawa International Center for Space Architecture, University of Houston College of Architecture Mission Enabling Capabilities • Delta-V Capability • Energy Management – Low Thrust/High Efficiency – Thermal Management • VASIMR – ISR Argon – Storage Capacity – High Thrust/Low Efficiency • Chemical Propellant – ISR Methane – Delivery Capacity & Methods – Aerobraking • Logistics – Gravity assist – Consumables • Energy Production – Expendables – Electrical – Recyclables – Chemical – In-Situ Producibles – Thermal – Transformables – Nuclear • Communications • Fuel (transportable Energy) – Satellites – Production • Solar Orbit – Storage • Mars Orbit – Transportation Sasakawa International Center for Space Architecture, University of Houston College of Architecture Mission Enabling Capabilities • Knowledge Capture • Command, Control and – High-speed Data Synchronization – Low rate Data Capability – Long Range • Payload Capability – Local Area Networks – The stuff that’s above and – Trans-Martian Network beyond what’s needed to – Cameras just get there and back – sensors – Discretionary mass with needs • Attitude Control – Provides end-products or • Navigation expanded capabilities – Intra-Planetary –Orbital –Surface Sasakawa International Center for Space Architecture, University of Houston College of Architecture Mission Enabling Capabilities • Robotic Capability • Surface Mobility –Scale – Stuff •Size – People • Quantity – Materials – Location – In-Situ Materials • Mars, Phobos & Deimos •Orbital • Telepresence •Surface – The ability to virtually – Interoperability and intra- transcend space operability • Human Presence Capability – Places to be, work, live, and survive – Abilities to transition between environments Sasakawa International Center for Space Architecture, University of Houston College of Architecture How We Achieve This Architecture Operational Phases – Precursor Reconnaissance Missions – Cargo/Infrastructure – Human Transfer – Operations in Martian System – Return Home Sasakawa International Center for Space Architecture, University of Houston College of Architecture Phase 1: Preliminary Missions • Satellites form communications infrastructure – Mars Orbiting – Solar Orbiting • Robotic missions characterize landing sites – Orbital Reconnaissance – Surface Missions • Sample return mission demonstrates ISRU Sasakawa International Center for Space Architecture, University of Houston College of Architecture Phase 2: Cargo Delivery • 20-30 Mt commercial launch vehicles • Autonomous rendezvous & docking • Propulsion – Chemical –Plasma • Braking into Mars orbit – Aerobraking – Propulsive deceleration Sasakawa International Center for Space Architecture, University of Houston College of Architecture Phase 3: Propellant Production and Systems Checkout • Begin multi-functional depot assembly in LMO • Deploy ISRU plant on Martian surface • Begin placing surface infrastructure • Test out mission architecture at all levels Sasakawa International Center for Space Architecture, University of Houston College of Architecture Phase 4: Crew Transfer • Minimize crew transfer time • Protect against radiation – Avoid Van Allen Belt – Use “storm shelters” peak events • VASIMR – Needs lots of power – Requires spiral out period Sasakawa International Center for Space Architecture, University of Houston College of Architecture Phase 5: Operations in Low Mars Orbit • Rendezvous with multi-functional depot • Begin exploration of Phobos • Tele-operation of near real-time rovers & robots Sasakawa International Center for Space Architecture, University of Houston College of Architecture Phase 6: Surface Operations • Flexible surface mission durations •ISRU – Oxygen for breathing – Oxygen used with hydrogen feedstock to create water – Oxygen used with methane for combustion Sasakawa International Center for Space Architecture, University of Houston College of Architecture Phase 7: Return Home • Methane and oxygen powered ascent vehicle • Rendezvous and docking with crew transfer vehicle • Argon VASIMR propulsion – 4 day Mars spiral and 85 day transit to Earth • Return to surface – Direct entry – LEO recovery Sasakawa International Center for Space Architecture, University of Houston College of Architecture Crew Operations Throughout • Housekeeping • Health maintenance • Science • Public outreach • Personal communications Sasakawa International Center for Space Architecture, University of Houston College of Architecture Crew Operations by Mission Phase • Outbound – Training – Maintenance • Mars Vicinity – Remote operations of robots – Observations – EVAs • Inbound – Debriefing – Analysis of samples Sasakawa International Center for Space Architecture, University of Houston College of Architecture Maintaining Public Interest •“Wow” Factor – Making it continuously interesting – Maintaining the return on investment in the form of value-added outposts – Keeping it sold • Vicarious Presence • Taking it to the people • Commercialization • Investment • Education outreach Sasakawa International Center for Space Architecture, University of Houston College of Architecture Architecture Elements Propulsion – James Doehring Depots – Michael Fehlinger Element Concepts – Frank Eichstadt LMO Command & Control Module – Kristine Ferrone Launch Vehicle Options – Loi Nguyen Sasakawa International Center for Space Architecture, University of Houston College
Load more

Recommended publications
  • 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]
  • Human Spaceflight Plans of Russia, China and India
    Presentation to the ASEB Committee on NASA Technology Roadmaps Panel on Human Health and Surface Exploration June 1, 2011 by Marcia S. Smith Space and Technology Policy Group, LLC Russia Extensive experience in human spaceflight First animal in space (1957), first man in space (1961), first woman in space (1963), first spacewalk (1965), first space station (1971) Seven successful space stations (Salyut 1, 3, 4, 5, 6, 7 and Mir) before partnering in International Space Station (ISS) No people beyond low Earth orbit (LEO), however For earth orbit, continues to rely on Soyuz, first launched in 1967, but upgraded many times and is key to ISS operations Designed space shuttle, Buran, but launched only once in automated mode (no crew) in 1988 06-01-2011 2 Russia (2) Existing reliable launch vehicles Proton is largest: 21 tons to LEO; 5.5 tons to geostationary transfer orbit (GTO) Attempts to build Saturn V-equivalent in 1960s and 1970s failed (N1 failed four times in four attempts 1969-1972) Energiya booster in 1980s only flew twice (1987 with Polyus and 1988 with Buran). Abandoned for financial reasons. Was 100 tons to LEO; 18-20 tons to GTO; 32 tons to lunar trajectory. RD-170 engines for Energiya’s strap-ons live on today in other forms for Zenit, Atlas V, and Angara (under development) 06-01-2011 3 Russia (3) Robotic planetary space exploration mixed Excellent success at – Moon (Luna and Lunokhod series, plus Zond circumlunar flights) Venus (Venera series) Halley’s Comet (Vega 1 and 2—also Venus) Jinxed at Mars More than a dozen failures in 1960s - 1970s Partial success with Phobos 2 in 1988 (Phobos 1 failed) Mars 96 failed to leave Earth orbit Phobos-Grunt scheduled for later this year; designed as sample return from Phobos (includes Chinese orbiter) 06-01-2011 4 Russia (4) Grand statements over decades about sending people to the Moon and Mars, but never enough money to proceed.
    [Show full text]
  • Dm{F©H {Anmoq©
    PSLV-C19 RISAT-1 PSLV-C21 GSAT-10 PSLV-C20 SARAL dm{f©H {anmoQ© ANNUAL REPORT Panoramic view of SARAL (top) and smaller satellites (below) attached to the fourth stage of PSLV-C20 dm{f©H {anmoQ© ANNUAL REPORT 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) programme for management of natural resources and various developmental projects across the country using space based imagery • Indigenous capability for 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, IRS 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
    [Show full text]
  • India's Surprise Plan to Send People to Space by 2022
    NEWS IN FOCUS HUMAN SPACEFLIGHT India’s surprise plan to send people to space by 2022 Expensive mission could divert scarce resources from more useful space programmes. BY SANJAY KUMAR “It is possible to do a very basic programme would be used in the event of a mission in a short period of time,” says John Logsdon, being aborted mid-launch. ISRO has devel- ndia has set an ambitious goal to send a space-policy specialist at George Washing- oped and successfully tested a reusable space people to space by 2022. The mission and ton University in Washington DC. If success- shuttle, which could transport and return its short timeline — announced by Prime ful, India would become the fourth country the astronauts. The agency’s Geosynchro- IMinister Narendra Modi— surprised many, to launch its own manned spacecraft, after nous Satellite Launch Vehicle (GSLV) Mark including the head of the country’s space the United States, Russia and China. III rocket will probably be used to launch agency. But some observ- the craft. “It came as a surprise to us,” said Kaila- ers say that India has “Human savadivoo Sivan, chair of the Indian Space a lot of work ahead of spaceflight CAN IT BE DONE? Research Organisation (ISRO). Although it and might struggle with adequate The agency will have to upgrade some of its Indian space enthusiasts have discussed to meet the deadline. risk cannot be technologies, and test them all for crewed sending people into orbit for more than a Others have criti- inexpensive.” missions, says Ajey Lele, a senior fellow with decade, the idea has not gained major politi- cized the government the Institute for Defence Studies and Analy- cal support until now.
    [Show full text]
  • Development of Space Launch Vehicles in India
    Astropolitics The International Journal of Space Politics & Policy ISSN: 1477-7622 (Print) 1557-2943 (Online) Journal homepage: http://www.tandfonline.com/loi/fast20 Development of Space Launch Vehicles in India Rajaram Nagappa To cite this article: Rajaram Nagappa (2016) Development of Space Launch Vehicles in India, Astropolitics, 14:2-3, 158-176, DOI: 10.1080/14777622.2016.1244877 To link to this article: http://dx.doi.org/10.1080/14777622.2016.1244877 Published online: 02 Dec 2016. Submit your article to this journal Article views: 132 View related articles View Crossmark data Full Terms & Conditions of access and use can be found at http://www.tandfonline.com/action/journalInformation?journalCode=fast20 Download by: [National Institute of Advanced Studies] Date: 02 August 2017, At: 23:16 ASTROPOLITICS 2016, VOL. 14, NOS. 2–3, 158–176 http://dx.doi.org/10.1080/14777622.2016.1244877 Development of Space Launch Vehicles in India Rajaram Nagappa National Institute of Advanced Studies, Bangalore, India ABSTRACT The Indian space program is a spacefaring success story with demonstrated capability in the design and building of applica- tion and scientific satellites, and the means to launch them into desired orbits. The end-to-end mission planning and execution capability comes with a high emphasis on self-reli- ance. Sounding rockets and small satellite launch vehicles provided the initial experience base for India. This experience was consolidated and applied to realize larger satellite launch vehicles. While many of the launch vehicle technologies were indigenously developed, the foreign acquisition of liquid pro- pulsion technologies did help in catalyzing the development efforts.
    [Show full text]
  • Isro Facts- Faq Tnpsc Group 2 Ot and Ccse -Iv
    ARUL IAS ACADEMY ISRO- FAQ ISRO FACTS- FAQ TNPSC GROUP 2 OT AND CCSE -IV Frequently Asked Questions 1. Who is considered as the "founding father" of Indian Space Programme? Dr Vikram A Sarabhai is considered as the founding father of space programmes in India. 2. When was ISRO formed? ISRO was formed on August 15, 1969. 3. When was Department of Space constituted? Department of Space (DOS) and the Space Commission were set up in 1972. ISRO was brought under DOS on June 1, 1972 4. What is the main objective of ISRO? The prime objective of ISRO is to develop space technology and its application to various national needs 5. How these Objectives are met? ISRO has established two major space systems, INSAT for communication, television broadcasting and meteorological services, and Indian Remote Sensing Satellites (IRS) system for resources monitoring and management. ISRO has developed two satellite launch vehicles, PSLV and GSLV, to place INSAT and IRS satellites in the required orbits. 6. Where the Satellites are made? Satellites are made at ISRO Satellite Centre (ISAC), Bangalore. 7. Where the Rockets / Launch vehicles are made? Rockets / Launch Vehicles are made at Vikram Sarabhai Space Centre (VSSC), Thiruvanathapuram. 8. From where are the rockets launched? ISRO's Launch facility is located at SDSC SHAR from where Launch Vehicles and Sounding Rockets are launched. Sounding rockets are also launched from TERLS at Thiruvananthapuram. 9. How can I order for Satellite data? You can get data from National Remote Sensing Centre (NRSC), Hyderabad. Visit the website: www.nrsc.gov.in for more details.
    [Show full text]
  • On a New Orbit the Space Progamme in India Started Off Modestly in the 1960S, but Has Taken Off on an Exciting Journey of Late
    Space On a new Orbit The space progamme in India started off modestly in the 1960s, but has taken off on an exciting journey of late. The recent launch of yet another satellite, writes Roshesh. P, establishes India’s emergence as a signifi cant space and satellite power DPA 40 NDIA steps across the threshold of its 60th year of Independence, fi rmly securing another milestone in Iadvancing its space technology. The September launch of the GSLV-F04 put into orbit the Insat 4CR satellite, not just taking India’s satellite launching capabili- ties a notch higher in the world market, but also augmenting the country’s booming television and telecommunica- tion sectors. The Insat 4CR satellite will for the next 10 years provide direct-to-home televi- sion broadcasting, video picture transmis- sions and digital satellite news-gathering services from its geo-stationary orbit. The launch is also a pointer to India’s ambition to be a signifi cant player in the race for the $2.5 billion global satellite launch business. Even as it celebrates the success of the GSLV-F04, the premiere national space agency — the Indian Space Research Organisation (ISRO) — is preparing the DPA launch of the fi rst GSLV-Mark III series. SCANNING THE SKIES: For ISRO, 2007 has been a resounding success in determining its capabilities in high-end technologies Slated for launch in early 2009, it will arm ISRO with the competence to launch four- domestic satellite by an indigenously built country to access super-specialty medical tonne payloads into geo-transfer orbit.
    [Show full text]
  • Science and Technology Crux Vol. 10
    aspirantforum.com ScienceNews and for Tech.Apr-June 2017 The Crux of The Hindu Vol. 10 News of Apr-June 17 Vol. 10 Important News in the field of Space Atomic Energy Environment and Ecology Health and Medicine Bio-Technology Computer and IT Defence Agriculture Miscellaneous aspirantforum.com: ASPIRANT FORUM : Vol. 10 Apr.-June Vol. AN INITIATIVE BY UPSC ASPIRANTS Visit Aspirantforum.com for guidance and study material for IAS Exam. aspirantforum.com Science and Tech. The Crux of The Hindu Vol. 10 News of Apr-June 17 Aspirant Forum is a Community for the UPSC Contents Civil Services (IAS) Aspirants, to discuss and debate the various things related to the exam. We welcome an active Space.........................................4 participation from the fellow members to enrich the Atomic Energy.........................18 knowledge of all. Environment and Ecology.......23 Health and Medicine...............32 Compiled and Edited by Karuna Thakur Shakeel Anwar Bio-Technology.......................40 Designed by: Computer and IT......................47 Anupam Rastogi Defence....................................50 Miscellaneous..........................53 The Science and Tech. Crux will be published online for free for every three months. We appreciate the friends and followers for apprepreciating our effort. For any queries, guidance needs and support, Please contact at: [email protected] You may also follow our website Aspirantforum.comaspirantforum.com for free online coaching and guidance for IAS Vol. 10 Apr.-June Vol. Visit Aspirantforum.com for guidance and study material for IAS Exam. aspirantforum.com Science and Tech. The Crux of The Hindu Vol. 10 News of Apr-June 17 About the ‘CRUX’ After the success of our monthly magazine The Crux of The Hindu and PIB, we are introducing a new and convenient product, to help the aspirants for various public services examinations.
    [Show full text]
  • Space India 2.0 Commerce, Policy, Security and Governance Perspectives
    Space India 2.0 Commerce, Policy, Security and Governance Perspectives Rajeswari Pillai Rajagopalan Narayan Prasad (Eds.) ISBN: 978-81-86818-28-2 Printed by: Mohit Enterprises © 2017 Observer Research Foundation. All rights reserved. No part of this publication may be reproduced or transmitted in any form or by any means without permission in writing from ORF. CONTENTS Foreword vii K Kasturirangan, former Chairman, ISRO Introduction xi Rajeswari Pillai Rajagopalan and Narayan Prasad I Space Commerce 1. Space 2.0 India: Leapfrogging Indian Space Commerce 1 Narayan Prasad 2. Traditional Space and NewSpace Industry in India: Current Outlook and Perspectives for the Future 11 Narayan Prasad 3. A Review of India’s Commercial Space Efforts 23 K R Sridhara Murthi 4. Exploring the Potential of Satellite Connectivity for Digital India 37 Neha Satak, Madhukara Putty, Prasad H L Bhat 5. Unlocking the Potential of Geospatial Data 51 Arup Dasgupta 6. Developing a Space Start-up Incubator to Build a NewSpace Ecosystem in India 71 Narayan Prasad 7. Electronic Propulsion & Launch Vehicles: Today and Beyond – An Indian Perspective 85 Rohan M Ganapathy, Arun Radhakrishnan and Yashas Karanam iv II Space Policy 8. Privatisation of Space in India and the Need for A Law 103 Kumar Abhijeet 9. SATCOM Policy: Bridging the Present and the Future 119 Ashok GV and Riddhi D’ Souza 10. A Review of India’s Geospatial Policy 141 Ranjana Kaul 11. Formation of PSLV Joint Venture: Legal Issues 151 Malay Adhikari 12. Exploring Space as an Instrument in India’s Foreign Policy & Diplomacy 165 Vidya Sagar Reddy III Space Security 13.
    [Show full text]
  • GSLV Mark III-D1 / GSAT-19 Mission
    GSLV MkIII-D1/GSAT-19 Mission The Mission GSLV MkIII-D1/GSAT-19 Mission is the first developmental flight of GSLV MkIII, a heavy lift launch vehicle, capable of lofting payloads up to 4,000 kg into Geosynchronous Transfer Orbit (GTO) and 10,000 kg into Low Earth Orbit (LEO). GSAT-19, a high throughput communication satellite is identified as the payload in this mission. This will be the heaviest satellite being launched from India till date. Launch of GSLV MkIII-D1 is planned from the Second Launch Pad at Satish Dhawan Space Centre, Sriharikota. Mission Specifications Orbit GTO Perigee 170 km Apogee 35975 km Inclination 21.5 degree GSLV MkIII-D1 at Second Launch Pad Payload Mass 3136 kg GSLV MkIII-D1 Stage Characteristics Parameters Stages Two S 200 L110 C25 Length (m) 26.2 21.39 13.545 Diameter (m) 3.2 4 4 Propellants Composite solid Hypergolic liquid Cryogenic Propellant Mass (t) 2 x 205 116 28 Stage Mass at 472 125 33 Lift-off (t) GSLV MkIII-D1/GSAT-19 Mission C25 Cryogenic Stage with 20 tonne thrust Cryogenic engine at stage Preparation Facility The C25 cryogenic stage carries about 28 tons of cryogenic propellants stored on-board at very low temperatures. It is integrated on top of the L110 core liquid stage. The ignition of C25 stage takes place 2 s after the separation of the L110 stage about 322 s after lift-off. The functioning duration of C25 is 643 s and this will facilitate the GSAT-19 carried on-board to reach the intended GTO.
    [Show full text]
  • Indian Space Programme - Achievements
    Indian Space Programme - Achievements (May 2014 to April 2018) Indian Space Research Organisation (ISRO) has completed 166 missions out of which 53 missions (23 Launch vehicle missions, 23 satellite missions & 7 technology demonstration missions) has been accomplished during the period May 2014 to April 2018. Launch Vehicles a) Polar Satellite Launch Vehicle (PSLV): During the period, PSLV has completed 17 flights and has successfully orbited 224 satellites of total mass 19.2 tonnes in orbit. PSLV has demonstrated end to end launch services by launching 202 satellites for international customers from 24 countries including 3 dedicated commercial launches. PSLV upper stage (PS4) restart capability has also been demonstrated which enables PSLV to inject multiple satellites in different orbits in same mission thereby making PSLV more versatile launcher. PSLV also created history by deploying 104 satellite in a single launch. This remarkable exploit was a new moment of pride for scientific, space community and the country. b) Geosynchronous Satellite Launch Vehicle (GSLV Mk-II): ISRO has demonstrated the reliability of indigenous cryogenic technology with the four consecutive successful flights of Geosynchronous Satellite Launch Vehicle (GSLV) with indigenous Cryogenic engine & stage. c) GSLV-Mark III: The first experimental flight of GSLV MKIII (LVM3-X) was successfully launched on December 18, 2014. The valuable data generated from the experimental mission was utilized to improve the robustness of the vehicle. The first developmental flight was successfully launched, in which a 3136 kg communication satellite (GSAT- 19) was injected into the Geosynchronous Transfer Orbit on June 05, 2017. GSAT-19 is the heaviest satellite launched with Indian launch vehicle.
    [Show full text]
  • REPORT of the WORKING GROUP on "SPACE" on the ELEVENTH FIVE YEAR PLAN PROPOSALS 2007-1 2
    REPORT OF THE WORKING GROUP ON "SPACE" on the ELEVENTH FIVE YEAR PLAN PROPOSALS 2007-12 for INDIAN SPACE PROGRAMME Indian Space Research Organisation Department of Space Bangalore - 560 094 Contents II Preface Highlights of the Plan proposal 1) 1. Overview of Indian Space Programme 1 11 loth Plan 2002-07: targets and achievements 3. Overall Vision and Programme Directions 1 4. ELEVENTH FIVE YEAR PUN2007-12 PROPOSALS I1 Approach and formulation process 13 Satellite Communications & Navigation 15 Earth Observation systems 32 Disaster Management Support 52 Space Transportation System 61 Space Science and Environment Studies 67 Atmospheric Science programme 82 Master Plan for utilisation of Space Technology 86 for North East Development of Space materials and components, 91 Industry interface, Academia interface, commercialization and International Co-operation. Organisation development and human resources 97 5. Mission Profile and Plan Outlay 100 Appendix A: Tenth Five Year Plan 2002-07: Targets and Achievements Appendix 8: Brief summary of discussions and recommendations xi-xvii of the working group meeting held on Aug 23, 2006. List of Tables Page No. Table 2.1 : Highlights of Tenth Plan 2002-07 achievements 8 Table 4.2.1 : Transponders buildup of INSATIGSAT system 28 During 11' plan period. Table 4.2.2 : Satellite Communication Missions of llthplan 29 Table 4.2.3 : IRNSS Mission planned during llthplan 31 Table 4.3.1 : Earth Observation Systems Missions 48 llthplan and planned spill over to 12~plan Table 4.3.2 : Thrust application projects identified for llth 5 1 Five year plan - Earth Observation Systems. Table 4.6.1 : Overview of Space Science Missions of llthplan 8 1 Table 5.1 : Budgetary Outlay for llthplan - Summary 105 Table 5.2 : Budgetary projections for llthplan - breakup 106 List of Ficfures Location 1.
    [Show full text]