6 Dec 2019 Is Interstellar Travel to an Exoplanet Possible?
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Modeling Super-Earth Atmospheres in Preparation for Upcoming Extremely Large Telescopes
Modeling Super-Earth Atmospheres In Preparation for Upcoming Extremely Large Telescopes Maggie Thompson1 Jonathan Fortney1, Andy Skemer1, Tyler Robinson2, Theodora Karalidi1, Steph Sallum1 1University of California, Santa Cruz, CA; 2Northern Arizona University, Flagstaff, AZ ExoPAG 19 January 6, 2019 Seattle, Washington Image Credit: NASA Ames/JPL-Caltech/T. Pyle Roadmap Research Goals & Current Atmosphere Modeling Selecting Super-Earths for State of Super-Earth Tool (Past & Present) Follow-Up Observations Detection Preliminary Assessment of Future Observatories for Conclusions & Upcoming Instruments’ Super-Earths Future Work Capabilities for Super-Earths M. Thompson — ExoPAG 19 01/06/19 Research Goals • Extend previous modeling tool to simulate super-Earth planet atmospheres around M, K and G stars • Apply modified code to explore the parameter space of actual and synthetic super-Earths to select most suitable set of confirmed exoplanets for follow-up observations with JWST and next-generation ground-based telescopes • Inform the design of advanced instruments such as the Planetary Systems Imager (PSI), a proposed second-generation instrument for TMT/GMT M. Thompson — ExoPAG 19 01/06/19 Current State of Super-Earth Detections (1) Neptune Mass Range of Interest Earth Data from NASA Exoplanet Archive M. Thompson — ExoPAG 19 01/06/19 Current State of Super-Earth Detections (2) A Approximate Habitable Zone Host Star Spectral Type F G K M Data from NASA Exoplanet Archive M. Thompson — ExoPAG 19 01/06/19 Atmosphere Modeling Tool Evolution of Atmosphere Model • Solar System Planets & Moons ~ 1980’s (e.g., McKay et al. 1989) • Brown Dwarfs ~ 2000’s (e.g., Burrows et al. 2001) • Hot Jupiters & Other Giant Exoplanets ~ 2000’s (e.g., Fortney et al. -
The Space Launch System for Exploration and Science. K
45th Lunar and Planetary Science Conference (2014) 2234.pdf THE SPACE LAUNCH SYSTEM FOR EXPLORATION AND SCIENCE. K. Klaus1, M. S. Elsperman1, B. B. Donahue1, K. E. Post1, M. L. Raftery1, and D. B. Smith1, 1The Boeing Company, 13100 Space Center Blvd, Houston TX 77059, [email protected], [email protected], [email protected], mi- [email protected], [email protected], [email protected]. Introduction: The Space Launch System (SLS) is same time which will simplify mission design and re- the most powerful rocket ever built and provides a duce launch costs. One of the key features of the SLS critical heavy-lift launch capability enabling diverse in cislunar space is performance to provide “dual-use”, deep space missions. This exploration class vehicle i.e. Orion plus 15t of any other payload. launches larger payloads farther in our solar system An opportunity exists to deliver payload to the lu- and faster than ever before. Available fairing diameters nar surface or lunar orbit on the unmanned 2017 range from 5 m to 10 m; these allow utilization of ex- MPCV/ SLS test flight (~4.5t of mass margin exists for isting systems which reduces development risks, size this flight). Concepts of this nature can be done for limitations and cost. SLS injection capacity shortens less than Discovery class mission budgets (~$450M) mission travel time. Enhanced capabilities enable a and may be done as a joint venture by the NASA Sci- variety of missions including human exploration, plan- ence Mission Directorate and Human Exploration Op- etary science, astrophysics, heliophysics, planetary erations Mission Directorate using the successful Lu- defense, Earth observaton and commercial space en- nar Reconnaissance Orbiter as a program model. -
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. -
NASA Exoplanet Exploration the Search for Habitable Worlds and for Life Beyond the Solar System
The Aerospace & Defense Forum San Fernando Valley Chapter December 12, 2017 Show Me the Planets! NASA Exoplanet Exploration The Search for Habitable Worlds and for Life Beyond the Solar System Dr. Gary H. Blackwood Manager, NASA Exoplanet Exploration Program Jet Propulsion Laboratory, California Institute of Technology December 12, 2017 Aerospace and Defense Forum, San Fernando Chapter, Sherman Oaks, CA CL#18-1463 © 2017 All rights reserved Artist concept of Kepler-16b What is an Exoplanet? Exoplanet – a planet that orbits another star Credit: Paramount 1 1 The Aerospace & Defense Forum San Fernando Valley Chapter December 12, 2017 NASA Centers and Facilities 2 KEY SCIENCE THEMES Discovering the Secrets of the Universe Searching for Life Elsewhere Safeguarding and Improving Life on Earth 3 2 The Aerospace & Defense Forum San Fernando Valley Chapter December 12, 2017 4 SEARCHING FOR LIFE ELSEWHERE MSL Curiosity 5 3 The Aerospace & Defense Forum San Fernando Valley Chapter December 12, 2017 SEARCHING FOR LIFE ELSEWHERE Vera Rubin Ridge 6 SEARCHING FOR LIFE ELSEWHERE Cassini Grand finale 7 4 The Aerospace & Defense Forum San Fernando Valley Chapter December 12, 2017 Exoplanet Exploration Credit: PHL@UPR, Arecibo, ESA/Hubble, NASA “All These Worlds are Yours…” - Arthur C. Clarke, 2010: Odyssey Two 8 Credit: SETI Institute 9 5 The Aerospace & Defense Forum San Fernando Valley Chapter December 12, 2017 NASA Exoplanet Exploration Program Astrophysics Division, NASA Science Mission Directorate NASA’s search for habitable planets and life beyond our solar system Program purpose described in 2014 NASA Science Plan 1. Discover planets around other stars 2. Characterize their properties 3. -
Solar System Exploration: a Vision for the Next Hundred Years
IAC-04-IAA.3.8.1.02 SOLAR SYSTEM EXPLORATION: A VISION FOR THE NEXT HUNDRED YEARS R. L. McNutt, Jr. Johns Hopkins University Applied Physics Laboratory Laurel, Maryland, USA [email protected] ABSTRACT The current challenge of space travel is multi-tiered. It includes continuing the robotic assay of the solar system while pressing the human frontier beyond cislunar space, with Mars as an ob- vious destination. The primary challenge is propulsion. For human voyages beyond Mars (and perhaps to Mars), the refinement of nuclear fission as a power source and propulsive means will likely set the limits to optimal deep space propulsion for the foreseeable future. Costs, driven largely by access to space, continue to stall significant advances for both manned and unmanned missions. While there continues to be a hope that commercialization will lead to lower launch costs, the needed technology, initial capital investments, and markets have con- tinued to fail to materialize. Hence, initial development in deep space will likely remain govern- ment sponsored and driven by scientific goals linked to national prestige and perceived security issues. Against this backdrop, we consider linkage of scientific goals, current efforts, expecta- tions, current technical capabilities, and requirements for the detailed exploration of the solar system and consolidation of off-Earth outposts. Over the next century, distances of 50 AU could be reached by human crews but only if resources are brought to bear by international consortia. INTRODUCTION years hence, if that much3, usually – and rightly – that policy goals and technologies "Where there is no vision the people perish.” will change so radically on longer time scales – Proverbs, 29:181 that further extrapolation must be relegated to the realm of science fiction – or fantasy. -
Deuterium – Tritium Pulse Propulsion with Hydrogen As Propellant and the Entire Space-Craft As a Gigavolt Capacitor for Ignition
Deuterium – Tritium pulse propulsion with hydrogen as propellant and the entire space-craft as a gigavolt capacitor for ignition. By F. Winterberg University of Nevada, Reno Abstract A deuterium-tritium (DT) nuclear pulse propulsion concept for fast interplanetary transport is proposed utilizing almost all the energy for thrust and without the need for a large radiator: 1. By letting the thermonuclear micro-explosion take place in the center of a liquid hydrogen sphere with the radius of the sphere large enough to slow down and absorb the neutrons of the DT fusion reaction, heating the hydrogen to a fully ionized plasma at a temperature of ~ 105 K. 2. By using the entire spacecraft as a magnetically insulated gigavolt capacitor, igniting the DT micro-explosion with an intense GeV ion beam discharging the gigavolt capacitor, possible if the space craft has the topology of a torus. 1. Introduction The idea to use the 80% of the neutron energy released in the DT fusion reaction for nuclear micro-bomb rocket propulsion, by surrounding the micro-explosion with a thick layer of liquid hydrogen heated up to 105 K thereby becoming part of the exhaust, was first proposed by the author in 1971 [1]. Unlike the Orion pusher plate concept, the fire ball of the fully ionized hydrogen plasma can here be reflected by a magnetic mirror. The 80% of the energy released into 14MeV neutrons cannot be reflected by a magnetic mirror for thermonuclear micro-bomb propulsion. This was the reason why for the Project Daedalus interstellar probe study of the British Interplanetary Society [2], the neutron poor deuterium-helium 3 (DHe3) reaction was chosen. -
Solar Orbiter Assessment Study and Model Payload
Solar Orbiter assessment study and model payload N.Rando(1), L.Gerlach(2), G.Janin(4), B.Johlander(1), A.Jeanes(1), A.Lyngvi(1), R.Marsden(3), A.Owens(1), U.Telljohann(1), D.Lumb(1) and T.Peacock(1). (1) Science Payload & Advanced Concepts Office, (2) Electrical Engineering Department, (3) Research and Scientific Support Department, European Space Agency, ESTEC, Postbus 299, NL-2200AG, Noordwijk, The Netherlands (4) Mission Analysis Office, European Space Agency, ESOC, Darmstadt, Germany ABSTRACT The Solar Orbiter mission is presently in assessment phase by the Science Payload and Advanced Concepts Office of the European Space Agency. The mission is confirmed in the Cosmic Vision programme, with the objective of a launch in October 2013 and no later than May 2015. The Solar Orbiter mission incorporates both a near-Sun (~0.22 AU) and a high-latitude (~ 35 deg) phase, posing new challenges in terms of protection from the intense solar radiation and related spacecraft thermal control, to remain compatible with the programmatic constraints of a medium class mission. This paper provides an overview of the assessment study activities, with specific emphasis on the definition of the model payload and its accommodation in the spacecraft. The main results of the industrial activities conducted with Alcatel Space and EADS-Astrium are summarized. Keywords: Solar physics, space weather, instrumentation, mission assessment, Solar Orbiter 1. INTRODUCTION The Solar Orbiter mission was first discussed at the Tenerife “Crossroads” workshop in 1998, in the framework of the ESA Solar Physics Planning Group. The mission was submitted to ESA in 2000 and then selected by ESA’s Science Programme Committee in October 2000 to be implemented as a flexi-mission, with a launch envisaged in the 2008- 2013 timeframe (after the BepiColombo mission to Mercury) [1]. -
A Free Spacecraft Simulation Tool
Orbiter: AFreeSpacecraftSimulationTool MartinSchweiger DepartmentofComputerScience UniversityCollegeLondon www.orbitersim.com 2nd ESAWorkshoponAstrodynamics ToolsandTechniques ESTEC,Noordwijk 13-15September2004 Contents • Overview • Scope • Limitations • SomeOrbiterfeatures: • Timepropagation • Gravitycalculation • Rigid-bodymodelandsuperstructures • OrbiterApplicationProgrammingInterface: • Concept • Orbiterinstrumentation • TheVESSELinterfaceclass • Newfeatures: • Air-breatingengines:scramjetdesign • Virtualcockpits • Newvisualeffects • Orbiterasateachingtool • Summaryandfutureplans • Demonstration Overview · Orbiterisareal-timespaceflightsimulationforWindowsPC platforms. · Modellingofatmosphericflight(launchandreentry), suborbital,orbitalandinterplanetarymissions(rendezvous, docking,transfer,swing-byetc.) · Newtonianmechanics,rigidbodymodelofrotation,basic atmosphericflightmodel. · Planetpositionsfrompublicperturbationsolutions.Time integrationofstatevectorsorosculatingelements. · Developedsince2000asaneducationalandrecreational applicationfororbitalmechanicssimulation. · WritteninC++,usingDirectXfor3-Drendering.Public programminginterfacefordevelopmentofexternalmodule plugins. · WithanincreasinglyversatileAPI,developmentfocusis beginningtoshiftfromtheOrbitercoreto3rd partyaddons. Scope · Launchsequencefromsurfacetoorbitalinsertion(including atmosphericeffects:drag,pressure-dependentengineISP...) · Orbitalmanoeuvres(alignmentoforbitalplane,orbit-to-orbit transfers,rendezvous) · Vessel-to-vesselapproachanddocking.Buildingof superstructuresfromvesselmodules(includingsimplerules -
Planetary Science with an Interstellar Probe
EPSC Abstracts Vol. 13, EPSC-DPS2019-262-2, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Planetary science with an Interstellar Probe Kathleen Mandt, Kirby Runyon, Ralph McNutt, Pontus Brandt, Michael Paul, and Abigail Rymer Johns Hopkins University Applied Physics Laboratory, Laurel, MD, USA, ([email protected]) Abstract a) The Heliosphere as a Habitable Astrosphere: Characterize the heliosphere and the The space science community has maintained an interstellar medium to understand other ongoing interest in exploration of interstellar space for astrospheres harboring potentially habitable several decades. In 2016, Congressional language stellar-exoplanetary environments. encouraged NASA to take the enabling steps for an b) Formation and Evolution of Planetary Interstellar scientific probe. In 2018, a study was Systems: Explore the properties of Dwarf initiated targeting 1000 AU within 50 years using Planets, KBO worlds, giant planets, and the current or near-term technology. The ultimate goal of large scale structure of the circum-solar debris this study is to define a mission that would be feasible disk. to launch in the 2030’s, enabling humanity to take the c) Early Evolution of Galaxies: Uncover the first explicit step in to interstellar space scientifically, diffuse extragalactic background light. technically and programmatically. Although the d) Exoplanet Context: Explore the worlds of our primary goal of an Interstellar Probe would be to solar system as exoplanets. understand the heliosphere and the very local interstellar medium (VLISM), a probe designed to exit the solar system and explore interstellar space 1.1 Kuiper Belt Objectives provides a prime opportunity for planetary science. -
Impact of Stellar Superflares on Planetary Habitability 3 Exoplanets (Atri 2017)
Draft version June 20, 2019 Typeset using LATEX preprint style in AASTeX62 Impact of Stellar Superflares on Planetary Habitability Yosuke A. Yamashiki,1, 2 Hiroyuki Maehara,3, 4 Vladimir Airapetian,5, 6 Yuta Notsu,7, 8, 9 Tatsuhiko Sato,10 Shota Notsu,11, 9 Ryusuke Kuroki,1 Keiya Murashima,12 Hiroaki Sato,13 Kosuke Namekata,9 Takanori Sasaki,9, 2 Thomas B. Scott,14 Hina Bando,12 Subaru Nashimoto,12 Fuka Takagi,15 Cassandra Ling,1 Daisaku Nogami,9, 2 and Kazunari Shibata16, 2 1Graduate School of Advanced Integrated Studies in Human Survivability, Kyoto University, Sakyo, Kyoto, Japan 2Unit of the Synergetic Studies for Space, Kyoto University, Sakyo, Kyoto, Japan 3Okayama Branch Office, Subaru Telescope, National Astronomical Observatory of Japan, NINS, Kamogata, Asakuchi, Okayama, Japan 4Okayama Observatory, Kyoto University, Kamogata, Asakuchi, Okayama, Japan 5NASA/GSFC/SEEC, Greenbelt, MD, USA 6American University, DC, USA 7Laboratory for Atmospheric and Space Physics, University of Colorado Boulder, Boulder, CO, USA 8National Solar Observatory, Boulder, CO, USA 9Department of Astronomy, Kyoto University, Sakyo, Kyoto, Japan 10Nuclear Science and Engineering Center Center, Japan Atomic Energy Agency (JAEA), Tokai, Ibaraki, Japan 11Leiden Observatory, Leiden University, Leiden, The Netherlands 12Faculty of Science, Kyoto University, Sakyo, Kyoto, Japan 13Faculty of Engineering, Kyoto University, Sakyo, Kyoto, Japan 14Interface Analysis Centre, University of Bristol, Bristol, UK 15Faculty of Agriculture, Kyoto University, Sakyo, Kyoto, Japan 16Astronomical Observatory, Kyoto University, Sakyo, Kyoto, Japan (Received 17 April 2019; Revised 26 May 2019; Accepted 16 June 2019) Submitted to ApJ ABSTRACT High-energy radiation caused by exoplanetary space weather events from planet- hosting stars can play a crucial role in conditions promoting or destroying habitability in addition to the conventional factors. -
Building and Maintaining the International Space Station (ISS)
/ Building and maintaining the International Space Station (ISS) is a very complex task. An international fleet of space vehicles launches ISS components; rotates crews; provides logistical support; and replenishes propellant, items for science experi- ments, and other necessary supplies and equipment. The Space Shuttle must be used to deliver most ISS modules and major components. All of these important deliveries sustain a constant supply line that is crucial to the development and maintenance of the International Space Station. The fleet is also responsible for returning experiment results to Earth and for removing trash and waste from the ISS. Currently, transport vehicles are launched from two sites on transportation logistics Earth. In the future, the number of launch sites will increase to four or more. Future plans also include new commercial trans- ports that will take over the role of U.S. ISS logistical support. INTERNATIONAL SPACE STATION GUIDE TRANSPORTATION/LOGISTICS 39 LAUNCH VEHICLES Soyuz Proton H-II Ariane Shuttle Roscosmos JAXA ESA NASA Russia Japan Europe United States Russia Japan EuRopE u.s. soyuz sL-4 proton sL-12 H-ii ariane 5 space shuttle First launch 1957 1965 1996 1996 1981 1963 (Soyuz variant) Launch site(s) Baikonur Baikonur Tanegashima Guiana Kennedy Space Center Cosmodrome Cosmodrome Space Center Space Center Launch performance 7,150 kg 20,000 kg 16,500 kg 18,000 kg 18,600 kg payload capacity (15,750 lb) (44,000 lb) (36,400 lb) (39,700 lb) (41,000 lb) 105,000 kg (230,000 lb), orbiter only Return performance -
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.