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CARMENES Input Catalogue of M Dwarfs IV. New Rotation Periods from Photometric Time Series
Astronomy & Astrophysics manuscript no. pk30 c ESO 2018 October 9, 2018 CARMENES input catalogue of M dwarfs IV. New rotation periods from photometric time series E. D´ıezAlonso1;2;3, J. A. Caballero4, D. Montes1, F. J. de Cos Juez2, S. Dreizler5, F. Dubois6, S. V. Jeffers5, S. Lalitha5, R. Naves7, A. Reiners5, I. Ribas8;9, S. Vanaverbeke10;6, P. J. Amado11, V. J. S. B´ejar12;13, M. Cort´es-Contreras4, E. Herrero8;9, D. Hidalgo12;13;1, M. K¨urster14, L. Logie6, A. Quirrenbach15, S. Rau6, W. Seifert15, P. Sch¨ofer5, and L. Tal-Or5;16 1 Departamento de Astrof´ısicay Ciencias de la Atm´osfera, Facultad de Ciencias F´ısicas,Universidad Complutense de Madrid, E-280140 Madrid, Spain; e-mail: [email protected] 2 Departamento de Explotaci´ony Prospecci´onde Minas, Escuela de Minas, Energ´ıay Materiales, Universidad de Oviedo, E-33003 Oviedo, Asturias, Spain 3 Observatorio Astron´omicoCarda, Villaviciosa, Asturias, Spain (MPC Z76) 4 Centro de Astrobiolog´ıa(CSIC-INTA), Campus ESAC, Camino Bajo del Castillo s/n, E-28692 Villanueva de la Ca~nada,Madrid, Spain 5 Institut f¨ur Astrophysik, Georg-August-Universit¨at G¨ottingen, Friedrich-Hund-Platz 1, D-37077 G¨ottingen, Germany 6 AstroLAB IRIS, Provinciaal Domein \De Palingbeek", Verbrandemolenstraat 5, B-8902 Zillebeke, Ieper, Belgium 7 Observatorio Astron´omicoNaves, Cabrils, Barcelona, Spain (MPC 213) 8 Institut de Ci`enciesde l'Espai (CSIC-IEEC), Campus UAB, c/ de Can Magrans s/n, E-08193 Bellaterra, Barcelona, Spain 9 Institut d'Estudis Espacials de Catalunya (IEEC), E-08034 Barcelona, Spain 10 -
Breakthrough Propulsion Study Assessing Interstellar Flight Challenges and Prospects
Breakthrough Propulsion Study Assessing Interstellar Flight Challenges and Prospects NASA Grant No. NNX17AE81G First Year Report Prepared by: Marc G. Millis, Jeff Greason, Rhonda Stevenson Tau Zero Foundation Business Office: 1053 East Third Avenue Broomfield, CO 80020 Prepared for: NASA Headquarters, Space Technology Mission Directorate (STMD) and NASA Innovative Advanced Concepts (NIAC) Washington, DC 20546 June 2018 Millis 2018 Grant NNX17AE81G_for_CR.docx pg 1 of 69 ABSTRACT Progress toward developing an evaluation process for interstellar propulsion and power options is described. The goal is to contrast the challenges, mission choices, and emerging prospects for propulsion and power, to identify which prospects might be more advantageous and under what circumstances, and to identify which technology details might have greater impacts. Unlike prior studies, the infrastructure expenses and prospects for breakthrough advances are included. This first year's focus is on determining the key questions to enable the analysis. Accordingly, a work breakdown structure to organize the information and associated list of variables is offered. A flow diagram of the basic analysis is presented, as well as more detailed methods to convert the performance measures of disparate propulsion methods into common measures of energy, mass, time, and power. Other methods for equitable comparisons include evaluating the prospects under the same assumptions of payload, mission trajectory, and available energy. Missions are divided into three eras of readiness (precursors, era of infrastructure, and era of breakthroughs) as a first step before proceeding to include comparisons of technology advancement rates. Final evaluation "figures of merit" are offered. Preliminary lists of mission architectures and propulsion prospects are provided. -
100 Closest Stars Designation R.A
100 closest stars Designation R.A. Dec. Mag. Common Name 1 Gliese+Jahreis 551 14h30m –62°40’ 11.09 Proxima Centauri Gliese+Jahreis 559 14h40m –60°50’ 0.01, 1.34 Alpha Centauri A,B 2 Gliese+Jahreis 699 17h58m 4°42’ 9.53 Barnard’s Star 3 Gliese+Jahreis 406 10h56m 7°01’ 13.44 Wolf 359 4 Gliese+Jahreis 411 11h03m 35°58’ 7.47 Lalande 21185 5 Gliese+Jahreis 244 6h45m –16°49’ -1.43, 8.44 Sirius A,B 6 Gliese+Jahreis 65 1h39m –17°57’ 12.54, 12.99 BL Ceti, UV Ceti 7 Gliese+Jahreis 729 18h50m –23°50’ 10.43 Ross 154 8 Gliese+Jahreis 905 23h45m 44°11’ 12.29 Ross 248 9 Gliese+Jahreis 144 3h33m –9°28’ 3.73 Epsilon Eridani 10 Gliese+Jahreis 887 23h06m –35°51’ 7.34 Lacaille 9352 11 Gliese+Jahreis 447 11h48m 0°48’ 11.13 Ross 128 12 Gliese+Jahreis 866 22h39m –15°18’ 13.33, 13.27, 14.03 EZ Aquarii A,B,C 13 Gliese+Jahreis 280 7h39m 5°14’ 10.7 Procyon A,B 14 Gliese+Jahreis 820 21h07m 38°45’ 5.21, 6.03 61 Cygni A,B 15 Gliese+Jahreis 725 18h43m 59°38’ 8.90, 9.69 16 Gliese+Jahreis 15 0h18m 44°01’ 8.08, 11.06 GX Andromedae, GQ Andromedae 17 Gliese+Jahreis 845 22h03m –56°47’ 4.69 Epsilon Indi A,B,C 18 Gliese+Jahreis 1111 8h30m 26°47’ 14.78 DX Cancri 19 Gliese+Jahreis 71 1h44m –15°56’ 3.49 Tau Ceti 20 Gliese+Jahreis 1061 3h36m –44°31’ 13.09 21 Gliese+Jahreis 54.1 1h13m –17°00’ 12.02 YZ Ceti 22 Gliese+Jahreis 273 7h27m 5°14’ 9.86 Luyten’s Star 23 SO 0253+1652 2h53m 16°53’ 15.14 24 SCR 1845-6357 18h45m –63°58’ 17.40J 25 Gliese+Jahreis 191 5h12m –45°01’ 8.84 Kapteyn’s Star 26 Gliese+Jahreis 825 21h17m –38°52’ 6.67 AX Microscopii 27 Gliese+Jahreis 860 22h28m 57°42’ 9.79, -
Download the Search for New Planets
“VITAL ARTICLES ON SCIENCE/CREATION” September 1999 Impact #315 THE SEARCH FOR NEW PLANETS by Don DeYoung, Ph.D.* The nine solar system planets, from Mercury to Pluto, have been much-studied targets of the space age. In general, a planet is any massive object which orbits a star, in our case, the Sun. Some have questioned the status of Pluto, mainly because of its small size, but it remains a full-fledged planet. There is little evidence for additional solar planets beyond Pluto. Instead, attention has turned to extrasolar planets which may circle other stars. Intense competition has arisen among astronomers to detect such objects. Success insures media attention, journal publication, and continued research funding. The Interest in Planets Just one word explains the intense interest in new planets—life. Many scientists are convinced that we are not alone in space. Since life evolved on Earth, it must likewise have happened elsewhere, either on planets or their moons. The naïve assumption is that life will arise if we “just add water”: Earth-like planet + water → spontaneous life This equation is falsified by over a century of biological research showing the deep complexity of life. Scarcely is there a fact more certain than that matter does not spring into life on its own. Drake Equation Astronomer Frank Drake pioneered the Search for ExtraTerrestrial Intelligence project, or SETI, in the 1960s. He also attempted to calculate the total number of planets with life. The Drake Equation in simplified form is: Total livable Probability of Planets with planets x evolution = evolved life *Don DeYoung, Ph.D., is an Adjunct Professor of Physics at ICR. -
Tímaákvarðanir Á Myrkvum Valinna Myrkvatvístirna Og Þvergöngum Fjarreikistjarna, Árin 2017-2018, Og Fjarlægðamælingar
Tímaákvarðanir á myrkvum valinna myrkvatvístirna, þvergöngum fjarreikistjarna og fjarlægðamælingar, árin 2017—2018 Snævarr Guðmundsson 2019 Náttúrustofa Suðausturlands Litlubrú 2, 780 Höfn í Hornafirði Nýheimar, Litlubrú 2 780 Höfn Í Hornafirði www.nattsa.is Skýrsla nr. Dagsetning Dreifing NattSA 2019-04 10. apríl 2019 Opin Fjöldi síðna 109 Tímaákvarðanir á myrkvum valinna myrkvatvístirna, Fjöldi mynda 229 þvergöngum fjarreikistjarna og fjarlægðamælingar, árin 2017- 2018. Verknúmer 1280 Höfundur: Snævarr Guðmundsson Verkefnið var styrkt af Prófarkarlestur Þorsteinn Sæmundsson, Kristín Hermannsdóttir og Lilja Jóhannesdóttir Útdráttur Hér er gert grein fyrir stjörnuathugunum á Hornafirði á árabilinu 2017 til loka árs 2018. Í flestum tilfellum voru viðfangsefnin óeiginlegar breytistjörnur, aðallega myrkvatvístirni, en einnig var fylgst með nokkrum fjarreikistjörnum. Í mælingum á myrkvatvístirnum og fjarreikistjörnum er markmiðið að tímasetja myrkva og þvergöngur. Einnig er sagt frá niðurstöðum á nándarstjörnunni Ross 248 og athugunum á lausþyrpingunni NGC 7790 og breytistjörnum í nágrenni hennar. Markmið mælinga á nándarstjörnu og lausþyrpingum er að meta fjarlægðir eða aðra eiginleika fyrirbæranna. Að lokum eru kynntar athuganir á litrófi nokkurra bjartra stjarna. Í samantektinni er sagt frá hverju viðfangsefni í sérköflum. Þessi samantekt er sú þriðja um stjörnuathuganir sem er gefin út af Náttúrustofu Suðausturlands. Niðurstöður hafa verið sendar í alþjóðlegan gagnagrunn þar sem þær, ásamt fjölda sambærilegra mæligagna frá stjörnuáhugamönnum, eru aðgengilegar stjarnvísindasamfélaginu. Hægt er að sækja skýrslur um stjörnuathuganir á vefslóðina: http://nattsa.is/utgefid-efni/. Lykilorð: myrkvatvístirni, fjarreikistjörnur, breytistjörnur, lausþyrpingar, ljósmælingar, fjarlægðir stjarna, litróf stjarna. ii Tímaákvarðanir á myrkvum valinna myrkvatvístirna, þvergöngum fjarreikistjarna og fjarlægðamælingar, árin 2017-2018. — Annáll 2017-2018. Timings of selected eclipsing binaries, exoplanet transits and distance measurements in 2017- 2018. -
E-Sail for Fast Interplanetary Travel. M
Planetary Science Vision 2050 Workshop 2017 (LPI Contrib. No. 1989) 8056.pdf E-SAIL FOR FAST INTERPLANETARY TRAVEL. M. Aru1, P. Janhunen2, 1University of Tartu, Estonia, 2Finnish Meteorological Institute, Finland Introduction: Propulsion is a significant factor for areas of scientific research and new types of missions our access to the Solar System and the time con- could be imagined and created, improving our unders- sumption of the missions. We propose to use the elect- tanding of the Solar System. ric solar wind sail (E-sail), which can provide remar- Manned presence on Mars. A spacecraft equipped kable low thrust propulsion without needing propellant with a large E-sail, that provides 1 N of thrust at 1 au [1, 2]. from Sun, can travel from Earth to the asteroid belt in a The E-sail is a propellantless propulsion concept year. One such spacecraft can bring back three tonnes that uses centrifugally stretched, charged tethers to of water in three years, and repeat the journey multiple extract momentum from the solar wind to produce times within its estimated lifetime of at least ten years thrust. Over periods of months, this small but conti- [9, 12]. The water can be converted to synthetic cryo- nuous thrust can accelerate the spacecraft to great genic rocket fuel in orbital fuelling stations where speeds of approximately 20 to 30 au/year. For examp- manned vehicles travelling between Earth and Mars le, distances of 100 au could be reached in <10 years, can be fuelled. This dramatically reduces the overall which is groundbreaking [1]. mission fuel ratio at launch, and opens up possibilities The principles of operation: A full-scale E-sail for affordable continuous manned presence on Mars includes up to 100 thin, many kilometers long tethers, [13]. -
IAF Space Propulsion Symposium 2019
IAF Space Propulsion Symposium 2019 Held at the 70th International Astronautical Congress (IAC 2019) Washington, DC, USA 21 -25 October 2019 Volume 1 of 2 ISBN: 978-1-7138-1491-7 Printed from e-media with permission by: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 Some format issues inherent in the e-media version may also appear in this print version. Copyright© (2019) by International Astronautical Federation All rights reserved. Printed with permission by Curran Associates, Inc. (2020) For permission requests, please contact International Astronautical Federation at the address below. International Astronautical Federation 100 Avenue de Suffren 75015 Paris France Phone: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 www.iafastro.org Additional copies of this publication are available from: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 USA Phone: 845-758-0400 Fax: 845-758-2633 Email: [email protected] Web: www.proceedings.com TABLE OF CONTENTS VOLUME 1 PROPULSION SYSTEM (1) BLUE WHALE 1: A NEW DESIGN APPROACH FOR TURBOPUMPS AND FEED SYSTEM ELEMENTS ON SOUTH KOREAN MICRO LAUNCHERS ............................................................................ 1 Dongyoon Shin KEYNOTE: PROMETHEUS: PRECURSOR OF LOW-COST ROCKET ENGINE ......................................... 2 Jérôme Breteau ASSESSMENT OF MON-25/MMH PROPELLANT SYSTEM FOR DEEP-SPACE ENGINES ...................... 3 Huu Trinh 60 YEARS DLR LAMPOLDSHAUSEN – THE EUROPEAN RESEARCH AND TEST SITE FOR CHEMICAL SPACE PROPULSION SYSTEMS ....................................................................................... 9 Anja Frank, Marius Wilhelm, Stefan Schlechtriem FIRING TESTS OF LE-9 DEVELOPMENT ENGINE FOR H3 LAUNCH VEHICLE ................................... 24 Takenori Maeda, Takashi Tamura, Tadaoki Onga, Teiu Kobayashi, Koichi Okita DEVELOPMENT STATUS OF BOOSTER STAGE LIQUID ROCKET ENGINE OF KSLV-II PROGRAM ....................................................................................................................................................... -
Interstellar Travel and the Fermi Paradox
Interstellar Travel If aliens haven’t visited us, could we go to them? In this lecture we will have some fun speculating about future interstellar travel by humans. Please keep in mind that, as we discussed earlier, this cannot be considered a solution for the problems that we have on Earth, for the simple reason that the expense per person is utterly prohibitive and will remain so in any conceivable future scenario. Nonetheless, given enough time it could be that we have the capacity to move out into the galaxy. Incidentally, we will leave discussions of really far-out concepts such as wormholes to a future class. Interstellar distances The major barrier to interstellar travel is the staggering distance between stars. The closest one to the Sun is Proxima Centauri, which is 4.3 light years away but not a likely host to planets. There are, however, a few possibilities within roughly 10 light years, so that is a good target. How far is 10 light years? By definition it is how far light travels in 10 years, but let’s put this into a more familiar context. A moderately brisk walking pace is 5 km/hr, and since one light year is about 10 trillion kilometers, you would need about 20 trillion hours, or about 2.3 billion years, to walk that distance. The fastest cars sold commercially go about 400 km/hr, so you would need about three billion hours or a bit less than thirty million years. The speed of the Earth in its orbit, which is comparable to the speed of the fastest spacecraft we have constructed (all unmanned, of course), is about 30 km/s and even at that rate it would take about a hundred thousand years to travel ten light years. -
Interstellar Travel Or Even 1.3 Mlbs at Launch
Terraforming Mars: By Aliens? Astronomy 330 •! Sometime movies are full of errors. •! But what can you do? Music: Rocket Man– Elton John Online ICES Question •! ICES forms are available online, so far 39/100 Are you going to fill out an ICES form before the students have completed it. deadline? •! I appreciate you filling them out! •! Please make sure to leave written comments. I a)! Yes, I did it already. find these comments the most useful, and typically b)! Yes, sometime today that’s where I make the most changes to the c)! Yes, this weekend course. d)! Yes, I promise to do it before the deadline of May6th! e)! No, I am way too lazy to spend 5 mins to help you or future students out. Final Final •! In this classroom, Fri, May 7th, 0800-1100. •! A normal-sized sheet of paper with notes on both •! Will consist of sides is allowed. –! 15 question on Exam 1 material. •! Exam 1and 2 and last year’s final are posted on –! 15 question on Exam 2 material. class website (not Compass). –! 30 questions from new material (Lect 20+). –! +4 extra credit questions •! I will post a review sheet Friday. •! A total of 105 points, i.e. 5 points of extra credit. •! Final Exam grade is based on all three sections. •! If Section 1/2 grade is higher than Exam 1/2 grade, then it will replace your Exam 1/2 grade. Final Papers Outline •! Final papers due at BEGINNING of discussion •! Rockets: how to get the most bang for the buck. -
Space Propulsion.Pdf
Deep Space Propulsion K.F. Long Deep Space Propulsion A Roadmap to Interstellar Flight K.F. Long Bsc, Msc, CPhys Vice President (Europe), Icarus Interstellar Fellow British Interplanetary Society Berkshire, UK ISBN 978-1-4614-0606-8 e-ISBN 978-1-4614-0607-5 DOI 10.1007/978-1-4614-0607-5 Springer New York Dordrecht Heidelberg London Library of Congress Control Number: 2011937235 # Springer Science+Business Media, LLC 2012 All rights reserved. This work may not be translated or copied in whole or in part without the written permission of the publisher (Springer Science+Business Media, LLC, 233 Spring Street, New York, NY 10013, USA), except for brief excerpts in connection with reviews or scholarly analysis. Use in connection with any form of information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed is forbidden. The use in this publication of trade names, trademarks, service marks, and similar terms, even if they are not identified as such, is not to be taken as an expression of opinion as to whether or not they are subject to proprietary rights. Printed on acid-free paper Springer is part of Springer Science+Business Media (www.springer.com) This book is dedicated to three people who have had the biggest influence on my life. My wife Gemma Long for your continued love and companionship; my mentor Jonathan Brooks for your guidance and wisdom; my hero Sir Arthur C. Clarke for your inspirational vision – for Rama, 2001, and the books you leave behind. Foreword We live in a time of troubles. -
Fusion Space Propulsion-A Shorter Time Frame Than You Think
FusionFusion SpaceSpace Propulsion--Propulsion-- AA ShorterShorter TimeTime FrameFrame thanthan YouYou ThinkThink JohnJohn F.F. SantariusSantarius FusionFusion TechnologyTechnology InstituteInstitute UniversityUniversity ofof WisconsinWisconsin JANNAFJANNAF Monterey,Monterey, 5-85-8 DecemberDecember 20052005 D-3He and Pulsed-Power Fusion Approaches Would Shorten Development Times $$$ Fusion D-3HeD-3He FRC,FRC, dipole,dipole, Rocket spheromak,spheromak, ST;ST; Pulsed-powerPulsed-power MTF,MTF, PHD,PHD, fast-ignitorfast-ignitor JFS 2005 Fusion Technology Institute 2 D-3He Fusion Will Provide Capabilities Not Available from Other Propulsion Options 107 Fusion ) s 6 / 10 10 kW/kg m ( y 1 kW/kg t i c o l 5 0.1 kW/kg e 10 v t Nuclear us (fission) Ga s-core fission ha electric x 4 E 10 Nuclear thermal Chemical 103 10-5 10-4 10-3 10-2 10-1 1 10 Thrust-to-weight ratio JFS 2005 Fusion Technology Institute 3 Predicted Specific Power of D-3He Magnetic Fusion Rockets Is Attractive (>1 kW/kg) • Predictions based on reasonably detailed magnetic fusion rocket studies. Specific Power First Author Year Configuration (kW/kg) Borowski 1987 Spheromak 10.5 Borowski 1987 Spherical torus 5.8 Santarius 1988 Tandem mirror 1.2 Bussard 1990 Riggatron 3.9 Teller 1991 Dipole 1.0 Nakashima 1994 Field-reversed configuration 1.0 Emrich 2000 Gasdynamic mirror 130 Thio 2002 Magnetized-target fusion 50 Williams 2003 Spherical torus 8.7 Cheung 2004 Colliding-beam FRC 1.5 JFS 2005 Fusion Technology Institute 4 Fusion Propulsion Would Enable Fast and Efficient Solar-System Travel • Fusion propulsion would dramatically reduce trip times (shown below) or increase payload fractions. -
Solar Electric Propulsion Sail
IOSR Journal of Electronics and Communication Engineering (IOSR-JECE) e-ISSN: 2278-2834,p- ISSN: 2278-8735.Volume 13, Issue 5, Ver. I (Sep.-Oct. 2018), PP 18-22 www.iosrjournals.org Solar Electric Propulsion Sail Dr. S.S. Subashka Ramesh [1] Sri Haripriya Nutulapti [2], Yashraj Sharma [3], Pratyush Kumar [4] [1], [2], [3], [4] Department of Computer Science and Engineering, SRM institute of science & technology Ramapuram Campus, Chennai-89, India. Corresponding Author: Dr. S.S. Subashka Ramesh Abstract: The solar expedition missions have been minimized mainly due to the performance of the space capsules, also because of the planned amount of fuel a space shuttle must carry without discharging in order to advance to an unfamiliar region. Traditionally, a solar electric propulsion sail is extremely deformable to drive a space rocket through outer space. Photon or electric sails are propounding medium of propulsion by utilizing the cosmic radiation endeavored because of sun’s rays on massive mirrors. It is a fusion of photo-voltaic cells and ions for the propelling and is also capable of enabling very fine maneuvering of the spacecraft by means of large sail-surface deformations. Solar electric propulsion sailutilizes the natural beams of sunlight to advancethe vehicles into and out of space, just the way wind helps to propel the sailboats over the water. NASA team claimed working on the start ofgrowth of technology on the assignment recognized as the solar sail demonstrator which proved thatmaking use of giant, weightless and unfurling objects float in universe would enhance the abilities of travelling deeper in space.