Exploration-Probe to Jupiter Moon Europa
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Sns College of Technology
SNS COLLEGE OF TECHNOLOGY (An Autonomous Institution) DEPARTMENT OF AERONAUTICAL ENGINEERING Subject Code & Name: 16AE409 ROCKETS AND MISSILES Date: 16.08.19 DAY: 01 UNIT: 4: STAGING OF ROCKETS AND MISSILES TOPIC: 1: TWO MARK QUESTION & ANSWER 1. Define multistage rocket. A multistage (or) multistep rocket is a series of individual vehicles or stages each with its own structure, tanks and engines. The stages are so connected that each operates in turn accelerating the remaining stages and the payload before being detached from them. 2. Nomenclature of the multistage rocket. 3. Write the different types of stage separation techniques. 1. By helical compression springs 2. By short duration solid propellant rockets. 4. Separation of stages with in the atmosphere The burnout of the first stage generally occurs within the upper region of the atmosphere i) Firing in the hole technique ii) Ullage rocket techniques. 5. Advantages of Multistage rocket design. Higher payload Enough to accelerate the initial mass Long-range Easy thrust programming K.NEHRU, M.Tech.,(Ph.D) Assistant Professor 16AE409 ROCKETS AND MISSILES 6. Write the expression for sub rocket 1 and (i+1). Sub rocket 1 = Complete rocket Sub rocket (i+1) = sub rocketi - stagei 7. Write the expression for payload of sub rocket 1 and N. Payload sub rocket i = Sub rocket (i+1) Payload sub rocket N = Actual payload 8. Sketch the thrust to time variation graph of stage separation techniques. i) Firing in the hole technique i) Ullage rocket techniques. 9. Drawbacks of firing in the hole techniques. K.NEHRU, M.Tech.,(Ph.D) Assistant Professor 16AE409 ROCKETS AND MISSILES 1. -
Semi Cryogenic Technology for Gaganyaan: RSTV – in Depth
Semi Cryogenic Technology for Gaganyaan: RSTV – In Depth Anchor: Teena Jha Context: India's strategic partner Russia has offered its Semi Cryogenic engine technology and critical components for the Gaganyaan project. Gaganyaan: In 2018, India’s first manned space mission was announced by Prime Minister Narendra Modi in his Independence Day speech. Gaganyaan will be the Indian crewed orbital spacecraft intended to be the basis of Indian Human Space Flight Program. With Gaganyaan, India will become only the 4th country after Russia, the USA and China to send humans to space. It will be ISRO’s next big project after the anticipated soft landing of Chandrayaan 2 on the lunar The target is to launch it before the 75 year celebration of India’s independence. Before the manned mission scheduled for December 2021, two unmanned tests will be carried out in December 2020 and July 2021. ISRO’s indigenous mission will be assisted by few other countries in selecting and training astronauts. According to ISRO, a budget of Rs 10,000 Cr. has been set aside for putting the infrastructure in place. It is described as a national mission than an ISRO mission. The Spacecraft: The spacecraft will take 3 Indian astronauts, who will be known as ‘vyomnauts’ (in Sanskrit ‘vyom’ means space. It will circle the earth for 7 days from a distance of 300-400 km. It will be launched by India’s biggest rocket GSLV Mk 3 from Sriharikotta. The 7 ton spacecraft will orbit the earth at an altitude of 400km for up to 7 days. -
3.1 Discipline Science Results
CASSINI FINAL MISSION REPORT 2019 1 SATURN Before Cassini, scientists viewed Saturn’s unique features only from Earth and from a few spacecraft flybys. During more than a decade orbiting the gas giant, Cassini studied the composition and temperature of Saturn’s upper atmosphere as the seasons changed there. Cassini also provided up-close observations of Saturn’s exotic storms and jet streams, and heard Saturn’s lightning, which cannot be detected from Earth. The Grand Finale orbits provided valuable data for understanding Saturn’s interior structure and magnetic dynamo, in addition to providing insight into material falling into the atmosphere from parts of the rings. Cassini’s Saturn science objectives were overseen by the Saturn Working Group (SWG). This group consisted of the scientists on the mission interested in studying the planet itself and phenomena which influenced it. The Saturn Atmospheric Modeling Working Group (SAMWG) was formed to specifically characterize Saturn’s uppermost atmosphere (thermosphere) and its variation with time, define the shape of Saturn’s 100 mbar and 1 bar pressure levels, and determine when the Saturn safely eclipsed Cassini from the Sun. Its membership consisted of experts in studying Saturn’s upper atmosphere and members of the engineering team. 2 VOLUME 1: MISSION OVERVIEW & SCIENCE OBJECTIVES AND RESULTS CONTENTS SATURN ........................................................................................................................................................................... 1 Executive -
GSLV Mk. II Launch Vehicle
Launch Vehicle Library Compiled by Patrick Blau GSLV Mk. II Launch Vehicle The Geosynchronous Satellite Launch Vehicle, better known by its abbreviation GSLV, is an Indian expendable launch system that was developed and is operated by the Indian Space Research Organization. The GSLV project was initiated back in the 1990s when India determined that it needed its own launch capability for Geosynchronous Satellites to become independent from other launch providers. At the time, India was relying on Russian/Soviet launch vehicles for heavy satellite launches. With the emergence of commercial launch providers, such as Arianespace, India shifted its GSO Satellites to those while GSLV was being developed. The launch system uses a large number of heritage components already employed on the Polar Satellite Launch Vehicle that first flew in 1993. The three-stage GSLV has an improved performance over four-stage PSLV with the addition of strap-on liquid-fueled boosters and a cryogenic upper stage. GSLV uses a combination of solid fueled, liquid-fueled and cryogenic stages. The vehicle weighs 414,000 Kilograms at liftoff standing 49 meters tall with a core diameter of 2.8 meters. The first stage is the S139 solid-fueled stage that is also used on PSLV. Around the core, four strap-on liquid-fueled boosters are mounted each featuring a Vikas engine using storable propellants. The second stage is also a storable propellant stage using a single modified Vikas engine while the third stage is a cryogenic stage using liquid Oxygen and liquid Hydrogen that is consumed by an ICE engine. The vehicle can deploy payloads of up to 2,500 Kilograms to a Geosynchronous Transfer Orbit, Low Earth Orbit Capability is 5,000kg. -
The Future Exploration of Saturn 417-441, in Saturn in the 21St Century (Eds. KH Baines, FM Flasar, N Krupp, T Stallard)
The Future Exploration of Saturn By Kevin H. Baines, Sushil K. Atreya, Frank Crary, Scott G. Edgington, Thomas K. Greathouse, Henrik Melin, Olivier Mousis, Glenn S. Orton, Thomas R. Spilker, Anthony Wesley (2019). pp 417-441, in Saturn in the 21st Century (eds. KH Baines, FM Flasar, N Krupp, T Stallard), Cambridge University Press. https://doi.org/10.1017/9781316227220.014 14 The Future Exploration of Saturn KEVIN H. BAINES, SUSHIL K. ATREYA, FRANK CRARY, SCOTT G. EDGINGTON, THOMAS K. GREATHOUSE, HENRIK MELIN, OLIVIER MOUSIS, GLENN S. ORTON, THOMAS R. SPILKER AND ANTHONY WESLEY Abstract missions, achieving a remarkable record of discoveries Despite the lack of another Flagship-class mission about the entire Saturn system, including its icy satel- such as Cassini–Huygens, prospects for the future lites, the large atmosphere-enshrouded moon Titan, the ’ exploration of Saturn are nevertheless encoura- planet s surprisingly intricate ring system and the pla- ’ ging. Both NASA and the European Space net s complex magnetosphere, atmosphere and interior. Agency (ESA) are exploring the possibilities of Far from being a small (500 km diameter) geologically focused interplanetary missions (1) to drop one or dead moon, Enceladus proved to be exceptionally more in situ atmospheric entry probes into Saturn active, erupting with numerous geysers that spew – and (2) to explore the satellites Titan and liquid water vapor and ice grains into space some of fi Enceladus, which would provide opportunities for which falls back to form nearly pure white snow elds both in situ investigations of Saturn’s magneto- and some of which escapes to form a distinctive ring sphere and detailed remote-sensing observations around Saturn (e.g. -
CASSINI Exploration of Saturn
CASSINI Exploration of Saturn Launch Location Cape Canaveral Air Force Station Launch Vehicle Titan IV-B Launch Date October 15, 1997 SATURN What do I see when I picture Saturn? Saturn is the sixth planet from the Sun and has been called “The Jewel of the Solar System.” Scientists be- lieve that Saturn formed more than four billion years ago from the same giant cloud of gas and dust whirling around the very young Sun that formed Earth and the other planets of our solar system. Saturn is much larg- er than Earth. Its mass is 95.18 times Earth’s mass. In other words, it would take over 95 Earths to equal the mass of Saturn. If you could weigh the planets on a giant scale, you would need slightly more than 95 Earths to equal the weight of Saturn. Saturn’s diameter is about 9.5 Earths across. At that ratio, if Saturn were as big as a baseball, Earth would be about half the size of a regular M&M candy. Saturn spins on its axis (rotates) just as our planet Earth spins on its axis. However, its period of rotation, or the time it takes Saturn to spin around one time, is only 10.2 Earth hours. A day on Saturn is just a little more than 10 hours long; so if you lived on Saturn, you would only have to be in school for a couple of hours each day! Because Saturn spins so fast, and its interior is gas, not rock, Saturn is noticeably flattened, top and bottom. -
In Situ Exploration of the Giant Planets Olivier Mousis, David H
In situ Exploration of the Giant Planets Olivier Mousis, David H. Atkinson, Richard Ambrosi, Sushil Atreya, Don Banfield, Stas Barabash, Michel Blanc, T. Cavalié, Athena Coustenis, Magali Deleuil, et al. To cite this version: Olivier Mousis, David H. Atkinson, Richard Ambrosi, Sushil Atreya, Don Banfield, et al.. In situ Exploration of the Giant Planets. 2019. hal-02282409 HAL Id: hal-02282409 https://hal.archives-ouvertes.fr/hal-02282409 Submitted on 2 Jun 2020 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. In Situ Exploration of the Giant Planets A White Paper Submitted to ESA’s Voyage 2050 Call arXiv:1908.00917v1 [astro-ph.EP] 31 Jul 2019 Olivier Mousis Contact Person: Aix Marseille Université, CNRS, LAM, Marseille, France ([email protected]) July 31, 2019 WHITE PAPER RESPONSE TO ESA CALL FOR VOYAGE 2050 SCIENCE THEME In Situ Exploration of the Giant Planets Abstract Remote sensing observations suffer significant limitations when used to study the bulk atmospheric composition of the giant planets of our solar system. This impacts our knowledge of the formation of these planets and the physics of their atmospheres. A remarkable example of the superiority of in situ probe measurements was illustrated by the exploration of Jupiter, where key measurements such as the determination of the noble gases’ abundances and the precise measurement of the helium mixing ratio were only made available through in situ measurements by the Galileo probe. -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2017) Publication produced for FAA AST by The Tauri Group under contract. NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY . -
Reliability Assessment of L40 Stage GSLV Mk II
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072 Reliability Assessment of L40 Stage GSLV Mk II Saureng Kumar1 1M.Tech, Dept. of Management Studies (Industrial Engineering & Management), IIT(ISM) Dhanbad, Jharkhand, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - Reliability of a component or system is the probability that a component or system will perform a required function for a given period of time when used under stated operating conditions. This paper discusses the reliability analysis of L 40 stage of Geosynchronous Satellite Launch Vehicle (GSLV Mk II). A variable mean time to failure rate model is also developed for analyzing observed failure data to ascertain probable cause. Key Words: System reliability, System Unreliability, Liquid Strap-on, Geosynchronous Satellite Launch Vehicle, Mean time to failure. 1. INTRODUCTION System reliability is a measurement science of a system or component to perform its intended function for a specific period of time under a given set of time. GSLV Mk II (Figure1) The first stage (GS1) comprises a solid propellant motor (S139) and four liquid strap-ons (L40). The designations of the different version indicate the type of fuel used and the mass of propellant booster strapped on to the rocket. “S” denotes “Solid” and the “L” denotes liquid and the second number represent mass (in ton) of propellant. The liquid strap-ons (L40) comprises 40 ton of liquid propellant powered by vikas engine with four identical separate steel tank, analysing the reliability of these subsystem and their Fig -1: Configuration Description relative contribution to spacecraft failures is important for reliability growth of spacecraft and targeted system Stage 1 improvements. -
Cassini-Huygens
High Ambitions for an Outstanding Planetary Mission: Cassini-Huygens Composite image of Titan in ultraviolet and infrared wavelengths taken by Cassini’s imaging science subsystem on 26 October. Red and green colours show areas where atmospheric methane absorbs light and reveal a brighter (redder) northern hemisphere. Blue colours show the high atmosphere and detached hazes (Courtesy of JPL /Univ. of Arizona) Cassini-Huygens Jean-Pierre Lebreton1, Claudio Sollazzo2, Thierry Blancquaert13, Olivier Witasse1 and the Huygens Mission Team 1 ESA Directorate of Scientific Programmes, ESTEC, Noordwijk, The Netherlands 2 ESA Directorate of Operations and Infrastructure, ESOC, Darmstadt, Germany 3 ESA Directorate of Technical and Quality Management, ESTEC, Noordwijk, The Netherlands Earl Maize, Dennis Matson, Robert Mitchell, Linda Spilker Jet Propulsion Laboratory (NASA/JPL), Pasadena, California Enrico Flamini Italian Space Agency (ASI), Rome, Italy Monica Talevi Science Programme Communication Service, ESA Directorate of Scientific Programmes, ESTEC, Noordwijk, The Netherlands assini-Huygens, named after the two celebrated scientists, is the joint NASA/ESA/ASI mission to Saturn Cand its giant moon Titan. It is designed to shed light on many of the unsolved mysteries arising from previous observations and to pursue the detailed exploration of the gas giants after Galileo’s successful mission at Jupiter. The exploration of the Saturnian planetary system, the most complex in our Solar System, will help us to make significant progress in our understanding -
Detection of Chemical Species in Titan's Atmosphere Using High
UNIVERSIDADE DE LISBOA FACULDADE DE CIÊNCIAS DEPARTAMENTO FÍSICA Detection of Chemical Species in Titan’s Atmosphere using High-Resolution Spectroscopy José Luís Fernandes Ribeiro Mestrado em Física Especialização em Astrofísica e Cosmologia Dissertação orientada por: Doutor Pedro Machado 2019 Acknowledgments This master’s thesis would not be possible without the support of my parents, Maria de F´atimaPereira Fernandes Ribeiro and Lu´ısCarlos Pereira Ribeiro, who I would like to thank for believing in me, encouraging me and allowing me to embark on this journey of knowledge and discovery. They made the person that I am today. I would like to thank all my friends and colleagues who accompanied me all these years for the great moments and new experiences that happened trough these years of university. They contributed a lot to my life and for that I am truly grateful. I just hope that I contributed to theirs as well. I also would like to thank John Pritchard from ESO Operations Support for helping me getting the EsoReflex UVES pipeline working on my computer, without him we would probably wouldn’t have the Titan spectra reduced by now. And I also like to thank Doctor Santiago P´erez-Hoyos for his availability to teach our planetary sciences group how to use the NEMESIS Radiative Transfer model and Doctor Th´er`ese Encrenaz for providing the ISO Saturn and Jupiter data. I would like to give a special thank you to Jo˜aoDias and Constan¸caFreire, for their support and help during this work. Lastly, and surely not the least, I would like to thank my supervisor Pedro Machado for showing me how to be a scientist and how to do scientific work. -
Kronos: Exploring the Depths of Saturn with Probes and Remote Sensing Through an International Mission
Exp Astron (2009) 23:947–976 DOI 10.1007/s10686-008-9094-9 ORIGINAL ARTICLE Kronos: exploring the depths of Saturn with probes and remote sensing through an international mission B. Marty & T. Guillot & A. Coustenis & the Kronos consortium & N. Achilleos & Y. Alibert & S. Asmar & D. Atkinson & S. Atreya & G. Babasides & K. Baines & T. Balint & D. Banfield & S. Barber & B. Bézard & G. L. Bjoraker & M. Blanc & S. Bolton & N. Chanover & S. Charnoz & E. Chassefière & J. E. Colwell & E. Deangelis & M. Dougherty & P. Drossart & F. M. Flasar & T. Fouchet & R. Frampton & I. Franchi & D. Gautier & L. Gurvits & R. Hueso & B. Kazeminejad & T. Krimigis & A. Jambon & G. Jones & Y. Langevin & M. Leese & E. Lellouch & J. Lunine & A. Milillo & P. Mahaffy & B. Mauk & A. Morse & M. Moreira & X. Moussas & C. Murray & I. Mueller-Wodarg & T. C. Owen & S. Pogrebenko & R. Prangé & P. Read & A. Sanchez-Lavega & P. Sarda & D. Stam & G. Tinetti & P. Zarka & J. Zarnecki Received: 7 December 2007 /Accepted: 2 April 2008 /Published online: 13 May 2008 # Springer Science + Business Media B.V. 2008 Abstract Kronos is a mission aimed to measure in situ the chemical and isotopic compositions of the Saturnian atmosphere with two probes and also by remote sensing, in order to understand the origin, formation, and evolution of giant planets in general, including extrasolar planets. The abundances of noble gases, hydrogen, B. Marty (*) CRPG, Nancy-Université, CNRS, BP 20, 54501 Vandoeuvre, Cedex, France e-mail: [email protected] T. Guillot Observatoire de la Côte d’Azur, BP 4229, 06304 Nice Cedex 04, France e-mail: [email protected] A.