Radioactive Waste Disposal in Space

Total Page:16

File Type:pdf, Size:1020Kb

Radioactive Waste Disposal in Space Radioactive waste disposal in space Technical, economic, legal issues and possible methods of solution INTERNATIONAL ACADEMY OF ASTRONAUTICS SUMMARY REPORT OF STUDY GROUP 3.21 VERSION 1.0 1 March, 2016 Contents ACRONYMS ............................................................................................................................................................................... 3 INTRODUCTION........................................................................................................................................................................ 4 1 NUCLEAR AND ENGINEERING ASPECTS OF RADIOACTIVE WASTE DISPOSAL IN SPACE ............................................. 5 1.1 GENERAL DESCRIPTION OF RADIOACTIVE WASTE PROBLEM AND ITS CURRENT STATE ..................................... 5 1.2 RAW MAIN ASPECTS AND MANAGEMENT STAGES ................................................................................................... 8 1.2.1 RAW AS A PART OF NUCLEAR FUEL CYCLE ....................................................................................................... 9 1.2.2 TRANSPORTATION EXPERIENCE ...................................................................................................................... 14 1.2.3 DEGREE OF RISK DURING SPENT FUEL TRANSPORTATION .......................................................................... 15 1.2.4 LIABILITY OF THE PARTIES DURING RAW MANAGEMENT .......................................................................... 16 1.3 RAW DISPOSAL METHODS ........................................................................................................................................ 16 1.3.1 GEOLOGICAL DISPOSAL ...................................................................................................................................... 19 1.3.2 WASTE DISPOSAL ON THE OCEAN FLOOR ....................................................................................................... 22 1.3.3 RAW DESTRUCTION BY NUCLEAR EXPLOSION .............................................................................................. 23 1.3.4 TRANSMUTATION ............................................................................................................................................... 23 1.3.5 RAW DISPOSAL IN SPACE ................................................................................................................................. 27 1.3.5.1 ISOTOPIC COMPOSITION OF DISPOSED RAW......................................................................................... 27 1.3.5.2 SEALED POWER CONTAINER .................................................................................................................... 34 2. ROCKET AND ENGINEERING ASPECTS OF RADIOACTIVE WASTE DISPOSAL IN SPACE ........................................... 37 2.1 SAFETY REQUIREMENTS ............................................................................................................................................ 37 2.2 DISPOSAL ORBIT SELECTION ..................................................................................................................................... 40 2.2.1 LAUNCH BASE SELECTION ................................................................................................................................. 41 2.2.2 GENERAL SEQUENCE OF OBJECT INJECTION INTO THE ORBIT OF THE ARTIFICIAL SUN SATELLITE ...... 41 2.2.3 SEQUENCE OF RAW INJECTION INTO OUTER RELATIVE TO THE EARTH DISPOSAL ORBIT .................... 43 2.2.4 RAW INJECTION INTO THE EARTH-SUN SYSTEM LIBRATION POINTS ....................................................... 46 2.3 SLV "MAYAK" USE ...................................................................................................................................................... 49 2.3.1 ERS OPERATION IN EMERGENCY SITUATIONS ............................................................................................... 54 2.3.2 PAYLOAD COMPOSITION ........................................................................................................................... 56 2.4 SLV "ZENIT-3SLBF" USE ......................................................................................................................................... 63 2.5 LIST OF POSSIBLE EMERGENCY SITUATIONS ........................................................................................................... 63 3 COST ASPECTS OF RADIOACTIVE WASTE DISPOSAL IN SPACE IN COMPARISON WITH ALTERNATIVE VARIANTS65 3.1 COSTS ............................................................................................................................................................................ 65 3.2 REVENUES .................................................................................................................................................................... 67 4 LEGAL ISSUES OF RAW DISPOSAL IN SPACE ................................................................................................................ 71 4.1 THE UNITED NATIONS ORGANIZATION .................................................................................................................. 71 4.2 THE INTERNATIONAL ATOMIC ENERGY AGENCY .................................................................................................. 79 4.3 OTHER INTERNATIONAL DOCUMENTS ..................................................................................................................... 80 4.4 THE UKRAINIAN LEGISLATION ................................................................................................................................. 82 5 COMPARATIVE EVALUATION OF RAW DISPOSAL IN SPACE IMPLEMENTATION VARIANTS .................................. 84 5.1 BRIEF CHARACTERISTIC OF MINIMUM TECHNICAL SOLUTIONS ........................................................................... 84 5.1.1 DISPOSAL OBJECT ............................................................................................................................................... 84 5.1.2 DISPOSAL SITE .................................................................................................................................................... 84 5.1.3 METHOD OF DELIVERY TO DISPOSAL SITE ...................................................................................................... 85 5.2 COMPARISON TECHNIQUE OF VARIANTS ................................................................................................................. 85 5.2.1 OPERATIONAL FEASIBILITY .............................................................................................................................. 86 ISKS Radioactive waste disposal in space Version | 1.0 01 March, 2016 5.2.2 R .................................................................................................................................................................... 86 1 2 5.2.3 IMPLEMENTATION PERIOD ............................................................................................................................... 87 5.2.4 COST ..................................................................................................................................................................... 87 5.2.5 PUBLIC ACCEPTANCE ......................................................................................................................................... 87 5.3 PROCESSING OF RESULTS ........................................................................................................................................... 89 REFERENCES ....................................................................................................................................................................... 92 6 POSSIBLE COOPERATION AND POTENTIAL CUSTOMERS ............................................................................................. 93 7 PROJECT SWOT ANALYSIS ............................................................................................................................................. 99 8 PROBLEMATIC ISSUES .................................................................................................................................................... 102 CONCLUSIONS ..................................................................................................................................................................... 104 SOURCES .............................................................................................................................................................................. 105 ANNEX 1 .............................................................................................................................................................................. 110 ANNEX 2 .............................................................................................................................................................................. 112 ANNEX 3 .............................................................................................................................................................................. 125 Radioactive waste disposal in space Version | 1.0 22 February, 2016 Acronyms AC - aerodynamic capsule NP - nuclear power NPP - nuclear power plant HAW - high-activity waste GEO - geostationary orbit SPC - sealed power container AES - artificial Earth satellite ASS - artificial Sun satellite SC - spacecraft
Recommended publications
  • A Doubly-Magic Storage Ring EDM Measurement Method
    A doubly-magic storage ring EDM measurement method Richard Talman Cornell University, Ithaca, U.S.A. 10 December, 2018 arXiv:1812.05949v1 [physics.acc-ph] 14 Dec 2018 1 Abstract This paper discusses \doubly-magic trap" operation of storage rings with su- perimposed electric and magnetic bending, allowing spins in two beams to be frozen (at the same time, if necessary), and their application to electric dipole moment (EDM) measurement. Especially novel is the possibility of simultaneous storage in the same ring of frozen spin beams of two different particle types. A few doubly-magic cases have been found: One has an 86.62990502 MeV frozen spin proton beam and a 30.09255159 MeV frozen spin positron beam (with accu- racies matching their known magnetic moments) counter-circulating in the same storage ring. (Assuming the positron EDM to be negligibly small) the positron beam can be used to null the worst source of systematic EDM error|namely, the existence of unintentional and unknown average radial magnetic field < Br > which, acting on the MDM, causes spurious background spin precession indis- tinguishable from foreground EDM-induced precession. The resulting measured proton minus positron EDM difference is then independent of < Br >. This amounts to being a measurement of the proton EDM. Most doubly-magic features can be tested in one or more \small" EDM proto- type rings. One promising example is a doubly-magic proton-helion combination, which would measure the difference between helion (i.e. helium-3) and proton EDM's. This combination can be used in the near future for EDM measurement, for example in a 10 m bending radius ring, using only already well-understood and proven technology.
    [Show full text]
  • Space in Central and Eastern Europe
    EU 4+ SPACE IN CENTRAL AND EASTERN EUROPE OPPORTUNITIES AND CHALLENGES FOR THE EUROPEAN SPACE ENDEAVOUR Report 5, September 2007 Charlotte Mathieu, ESPI European Space Policy Institute Report 5, September 2007 1 Short Title: ESPI Report 5, September 2007 Editor, Publisher: ESPI European Space Policy Institute A-1030 Vienna, Schwarzenbergplatz 6 Austria http://www.espi.or.at Tel.: +43 1 718 11 18 - 0 Fax - 99 Copyright: ESPI, September 2007 This report was funded, in part, through a contract with the EUROPEAN SPACE AGENCY (ESA). Rights reserved - No part of this report may be reproduced or transmitted in any form or for any purpose without permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “source: ESPI Report 5, September 2007. All rights reserved” and sample transmission to ESPI before publishing. Price: 11,00 EUR Printed by ESA/ESTEC Compilation, Layout and Design: M. A. Jakob/ESPI and Panthera.cc Report 5, September 2007 2 EU 4+ Executive Summary ....................................................................................... 5 Introduction…………………………………………………………………………………………7 Part I - The New EU Member States Introduction................................................................................................... 9 1. What is really at stake for Europe? ....................................................... 10 1.1. The European space community could benefit from a further cooperation with the ECS ................................................................. 10 1.2. However, their economic weight remains small in the European landscape and they still suffer from organisatorial and funding issues .... 11 1.2.1. Economic weight of the ECS in Europe ........................................... 11 1.2.2. Reality of their impact on competition ............................................ 11 1.2.3. Foreign policy issues ................................................................... 12 1.2.4. Internal challenges ..................................................................... 12 1.3.
    [Show full text]
  • Forward Helion Scattering and Neutron Polarization N
    Forward Helion Scattering and Neutron Polarization N. H. Buttimore Trinity College Dublin, Ireland Abstract. The elastic scattering of spin half helium-3 nuclei at small angles can show a sufficiently large analyzing power to enable the level of helion polarization to be evaluated. As the helion to a large extent inherits the polarization of its unpaired neutron the asymmetry observed in helion collisions can be transformed into a measurement of the polarization of its constituent neutron. Neutron polarimetry therefore relies upon understanding the spin dependence of the electromagnetic and hadronic interactions in the region of interference where there is an optimal analyzing power. Keywords: Neutron, spin polarization, helion, elastic scattering, asymmetry PACS: 11.80.Cr, 12.20.Ds, 13.40.Ks, 25.55.Ci, 13.85.Dz, 13.88.+e INTRODUCTION The spin polarized neutrons available from a polarized helium-3 beam would be very suitable for the study of polarized down quarks in various QCD processes particularly relating to transversity [1], nucleon spin structure [2], multi Pomeron exchange [3], gluon distributions [4], and additional dimensions [5]. Measuring the analyzing power in small angle elastic scattering of hadrons with spin provides an opportunity for evaluating the level of polarisation of incident helium-3 nuclei (helions) [6] thereby providing an effective neutron polarimeter [7]. Such a method relies upon an understanding of high energy spin dependence in diffractive processes [8]. Here, the interference of elastic hadronic and electromagnetic interactions in a suitable peripheral region enhances the size of the transverse spin asym- metry sufficiently to offer a tangible polarimeter for high energy helions.
    [Show full text]
  • The European Launchers Between Commerce and Geopolitics
    The European Launchers between Commerce and Geopolitics Report 56 March 2016 Marco Aliberti Matteo Tugnoli Short title: ESPI Report 56 ISSN: 2218-0931 (print), 2076-6688 (online) Published in March 2016 Editor and publisher: European Space Policy Institute, ESPI Schwarzenbergplatz 6 • 1030 Vienna • Austria http://www.espi.or.at Tel. +43 1 7181118-0; Fax -99 Rights reserved – No part of this report may be reproduced or transmitted in any form or for any purpose with- out permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “Source: ESPI Report 56; March 2016. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, inciden- tal or consequential, resulting from the information contained in this publication. Design: Panthera.cc ESPI Report 56 2 March 2016 The European Launchers between Commerce and Geopolitics Table of Contents Executive Summary 5 1. Introduction 10 1.1 Access to Space at the Nexus of Commerce and Geopolitics 10 1.2 Objectives of the Report 12 1.3 Methodology and Structure 12 2. Access to Space in Europe 14 2.1 European Launchers: from Political Autonomy to Market Dominance 14 2.1.1 The Quest for European Independent Access to Space 14 2.1.3 European Launchers: the Current Family 16 2.1.3 The Working System: Launcher Strategy, Development and Exploitation 19 2.2 Preparing for the Future: the 2014 ESA Ministerial Council 22 2.2.1 The Path to the Ministerial 22 2.2.2 A Look at Europe’s Future Launchers and Infrastructure 26 2.2.3 A Revolution in Governance 30 3.
    [Show full text]
  • F, I3/ M EARTH VIEW: a Business Guide to Orbital Remote Sensing
    _Ot-//JJ J zJ v - _'-.'3 7 F, i3/ m EARTH VIEW: A Business Guide to Orbital Remote Sensing NgI-Z4&71 (_!ASA-C_-ISB23_) EAsT VIEW: A 3USINESS GUI_E TO ORBITAL REMOTE SENSING (Houston Univ.) 13I p CSCL OBB Unclos G3/_3 001_137 Peter C. Bishop July 1990 Cooperative Agreement NCC 9-16 Research Activity No. IM.1 NASA Johnson Space Center Office of Commercial Programs Space Station Utilization Office "=.,. © Research Institute for Computing and Information Systems University of Houston - Clear Lake - T.E.C.H.N.I.C.A.L R.E.P.O.R.T Iml i I Jg. I k . U I i .... 7X7 iml The university of Houston-Clear Lake established the Research Institute for Computing and Information systems in 1986 to encourage NASA Johnson Space Center and local industry to actively support research in the computing and r' The information sciences. As part of this endeavor, UH-Clear Lake proposed a _._ partnership with JSC to jointly define and manage an integrated program of research in advanced data processing technology needed for JSC's main missions, including RICIS administrative, engineering and science responsibilities. JSC agreed and entered itffo : " a three-year cooperatlveagreement with UH-Clear _ke beginning in May, 1986, to ii jointly plan and execute such research through RICIS. Additionally, under Concept Cooperative Agreement NCC 9-16, computing and educational facilities are shared by the two institutions to conduct the research. The mission of RICIS is to conduct, coordinate and disseminate research on _-.. -- : computing and information systems among researchers, sponsors and users from UH-Clear Lake, NASA/JSC, and other research organizations.
    [Show full text]
  • Small-Scale Fusion Tackles Energy, Space Applications
    NEWS FEATURE NEWS FEATURE Small-scalefusiontacklesenergy,spaceapplications Efforts are underway to exploit a strategy that could generate fusion with relative ease. M. Mitchell Waldrop, Science Writer On July 14, 2015, nine years and five billion kilometers Cohen explains, referring to the ionized plasma inside after liftoff, NASA’s New Horizons spacecraft passed the tube that’s emitting the flashes. So there are no the dwarf planet Pluto and its outsized moon Charon actual fusion reactions taking place; that’s not in his at almost 14 kilometers per second—roughly 20 times research plan until the mid-2020s, when he hopes to faster than a rifle bullet. be working with a more advanced prototype at least The images and data that New Horizons pains- three times larger than this one. takingly radioed back to Earth in the weeks that If that hope pans out and his future machine does followed revealed a pair of worlds that were far more indeed produce more greenhouse gas–free fusion en- varied and geologically active than anyone had ergy than it consumes, Cohen and his team will have thought possible. The revelations were breathtak- beaten the standard timetable for fusion by about a ing—and yet tinged with melancholy, because New decade—using a reactor that’s just a tiny fraction of Horizons was almost certain to be both the first and the size and cost of the huge, donut-shaped “tokamak” the last spacecraft to visit this fascinating world in devices that have long devoured most of the research our lifetimes. funding in this field.
    [Show full text]
  • Space Technology and Telecommunication" Cluster of the Skolkovo Foundation
    STRATEGIC DIRECTIONS AND PRIORITY AREAS OF DEVELOPMENT FOR "S PACE TECHNOLOGY AND TELECOMMUNICATION " CLUSTER OF THE SKOLKOVO FOUNDATION 2012 Strategic Directions and Priority Areas of Development for "Space Technology and Telecommunication" Cluster of the Skolkovo Foundation The present document describes the results of methodology development and evaluation of strategic directions and priority areas for "Space Technology and Telecommunication" Cluster of the Skolkovo Fund. The first iteration was obtained by ST&T expert group with assistance of leading space R&D institutes using the Federal Space Agency materials. The Strategic Directions will be subsequently specified under the foresight research based on the contract between the Skolkovo Fund and one of the leading R&D and consulting organizations in the field of space activity and its results' commercialization. The Glossary can be found at the end of the document EXECUTIVE SUMMARY: PRIORITIES ST&T Cluster ensures search for, attraction and selection of potential subjects of innovative process in the field of development and target use of spacecrafts operation and diversification of rocket and space industry potential, facilitates their cooperation and provides the environment for full cycle innovation process establishment, based on the Strategic directions and priority areas of development, initially defined by this document and regularly updated considering opinion of sci-tech and business community that is identified in process of foresight procedure. At the moment, the Cluster finds it necessary, along with comprehensive support for innovative activity of the Skolkovo Fund participants and applicants, to focus on proactive implementation of several priority areas which particularly include: Establishing national infrastructure of full cycle microsatellite technology which involves leading universities.
    [Show full text]
  • Les Déchets Dans L'espace
    Les déchets dans l’espace 1 1 J i 0 u n 2 SOMMAIRE Introduction …………………………………………………………………………………. 3 I- Le milieu spatial …………………………………………………………………………. 5 II- Les déchets spatiaux …………………………………………………………………… 6 n°1 : Les lanceurs …………………………………………………………... 6 n°2 : Les résidus de combustion ……………………………………..….... 6 n°3 : Les déchets d’exploitation …………………………………………... 7 n°4 : Les Satellites Hors d’Usage …………………………………….…... 7 n°5 : Les déchets de fragmentation ………………………………….…... 8 5a- Explosions accidentelles ………………………………….…... 8 5b- Collisions accidentelles …………………………………...…... 8 5c- Destructions volontaires …………………………………..…... 9 n°6 : L’érosion spatiale ………………………………………………..…... 10 III- Inventaires des déchets spatiaux ………………………………………………..…... 11 1- Déchets en catalogue …………………………………………………... 11 2- Déchets hors catalogue …………………………………………….…... 13 IV- Les orbites basses (Low Earth Orbit, LEO) ………………………………………... 14 1- Trafic ……………………………………………………………………... 14 2- Satellites en activité, fonctions, nationalités ……………………...…... 14 3- La Station Spatiale Internationale (ISS) ………………………….…... 17 4- Les déchets en orbites basses …………………………………….…... 20 5- Les déchets de l’ISS (International Space Station) ……………..…... 22 V- Les orbites moyennes (Medium Earth Orbit, MEO) ………………………………... 26 1- Trafic ……………………………………………………………………... 26 2- Satellites en activité, fonctions, nationalités ……………………..…... 26 3- Les déchets en orbites moyennes ………………………………..…... 26 4- Les pelotes d’aiguilles de West-Ford ……………………………..…... 27 VI- L’orbite géostationnaire (Geostationary
    [Show full text]
  • Failures in Spacecraft Systems: an Analysis from The
    FAILURES IN SPACECRAFT SYSTEMS: AN ANALYSIS FROM THE PERSPECTIVE OF DECISION MAKING A Thesis Submitted to the Faculty of Purdue University by Vikranth R. Kattakuri In Partial Fulfillment of the Requirements for the Degree of Master of Science in Mechanical Engineering August 2019 Purdue University West Lafayette, Indiana ii THE PURDUE UNIVERSITY GRADUATE SCHOOL STATEMENT OF THESIS APPROVAL Dr. Jitesh H. Panchal, Chair School of Mechanical Engineering Dr. Ilias Bilionis School of Mechanical Engineering Dr. William Crossley School of Aeronautics and Astronautics Approved by: Dr. Jay P. Gore Associate Head of Graduate Studies iii ACKNOWLEDGMENTS I am extremely grateful to my advisor Prof. Jitesh Panchal for his patient guidance throughout the two years of my studies. I am indebted to him for considering me to be a part of his research group and for providing this opportunity to work in the fields of systems engineering and mechanical design for a period of 2 years. Being a research and teaching assistant under him had been a rewarding experience. Without his valuable insights, this work would not only have been possible, but also inconceivable. I would like to thank my co-advisor Prof. Ilias Bilionis for his valuable inputs, timely guidance and extremely engaging research meetings. I thank my committee member, Prof. William Crossley for his interest in my work. I had a great opportunity to attend all three courses taught by my committee members and they are the best among all the courses I had at Purdue. I would like to thank my mentors Dr. Jagannath Raju of Systemantics India Pri- vate Limited and Prof.
    [Show full text]
  • Russia and the Arms Trade
    Russia and the Arms Trade Stockholm International Peace Research Institute SIPRI is an independent international institute for research into problems of peace and conflict, especially those of arms control and disarmament. It was established in 1966 to commemorate Sweden’s 150 years of unbroken peace. The Institute is financed mainly by the Swedish Parliament. The staff and the Governing Board are international. The Institute also has an Advisory Committee as an international consultative body. The Governing Board is not responsible for the views expressed in the publications of the Institute. Governing Board Professor Daniel Tarschys, Chairman (Sweden) Dr Oscar Arias Sánchez (Costa Rica) Sir Marrack Goulding (United Kingdom) Dr Ryukichi Imai (Japan) Dr Catherine Kelleher (United States) Dr Marjatta Rautio (Finland) Dr Lothar Rühl (Germany) Dr Abdullah Toukan (Jordan) The Director Director Dr Adam Daniel Rotfeld (Poland) Stockholm International Peace Research Institute Frösunda, S-169 70 Solna Sweden Telephone: 46 8/655 97 00 Telefax: 46 8/655 97 33 Email: [email protected] Internet URL: http://www.sipri.se Russia and the Arms Trade Edited by Ian Anthony OXFORD UNIVERSITY PRESS 1998 Oxford University Press, Great Clarendon Street, Oxford OX2 6DP Oxford New York Athens Auckland Bangkok Bogotá Bombay Buenos Aires Calcutta Cape Town Dar es Salaam Delhi Florence Hong Kong Istanbul Karachi Kuala Lumpur Madras Madrid Melbourne Mexico City Nairobi Paris Singapore Taipei Tokyo Toronto Warsaw and associated companies in Berlin Ibadan Oxford is a registered trade mark of Oxford University Press Published in the United States by Oxford University Press Inc., New York © SIPRI 1998 All rights reserved.
    [Show full text]
  • The Regulation of Fusion – a Practical and Innovation-Friendly Approach
    The Regulation of Fusion – A Practical and Innovation-Friendly Approach February 2020 Amy C. Roma and Sachin S. Desai AUTHORS Amy C. Roma Sachin S. Desai Partner, Washington, D.C. Senior Associate, Washington, D.C. T +1 202 637 6831 T +1 202 637 3671 [email protected] [email protected] The authors want to sincerely thank the many stakeholders who provided feedback on this paper, and especially William Regan for his invaluable contributions and review of the technical discussion. TABLE OF CONTENTS I. EXECUTIVE SUMMARY 1 II. THE STATE OF FUSION INNOVATION 3 A) An Introduction to Fusion Energy 3 B) A Rapid Growth in Private-Sector Fusion Innovation 4 III. U.S. REGULATION OF ATOMIC ENERGY - NOT ONE SIZE FITS ALL 7 A) The Foundation of U.S. Nuclear Regulation - The Atomic Energy Act and the NRC 7 B) The Atomic Energy Act Embraces Different Regulations for Different Situations 7 1. NRC Frameworks for Different Safety Cases 8 2. Delegation of Regulatory Authority to States 9 IV. THE REGULATION OF FUSION - A PRACTICAL AND INNOVATION- FRIENDLY APPROACH 10 A) Fusion Regulation Comes to the Fore, Raising Key Questions 10 B) A Regulatory Proposal That Recognizes the Safety Case of Fusion and the Needs of Fusion Innovators 11 1. Near-Term: Regulation of Fusion Under the Part 30 Framework is Appropriate Through Development and Demonstration 11 2. Long-Term: The NRC Should Develop an Independent Regulatory Framework for Fusion at Commercial Scale, Not Adopt a Fission Framework 12 V. CONCLUSION 14 1 Hogan Lovells I. EXECUTIVE SUMMARY Fusion, the process that powers the Sun, has long been seen Most fusion technologies are already regulated by the NRC as the “holy grail” of energy production.
    [Show full text]
  • Fundamental Physical Constants — Complete Listing Relative Std
    From: http://physics.nist.gov/constants Fundamental Physical Constants — Complete Listing Relative std. Quantity Symbol Value Unit uncert. ur UNIVERSAL 1 speed of light in vacuum c; c0 299 792 458 m s− (exact) 7 2 magnetic constant µ0 4π 10− NA− × 7 2 = 12:566 370 614::: 10− NA− (exact) 2 × 12 1 electric constant 1/µ0c "0 8:854 187 817::: 10− F m− (exact) characteristic impedance × of vacuum µ / = µ c Z 376:730 313 461::: Ω (exact) p 0 0 0 0 Newtonian constant 11 3 1 2 3 of gravitation G 6:673(10) 10− m kg− s− 1:5 10− × 39 2 2 × 3 G=¯hc 6:707(10) 10− (GeV=c )− 1:5 10− × 34 × 8 Planck constant h 6:626 068 76(52) 10− J s 7:8 10− × 15 × 8 in eV s 4:135 667 27(16) 10− eV s 3:9 10− × 34 × 8 h=2π ¯h 1:054 571 596(82) 10− J s 7:8 10− × 16 × 8 in eV s 6:582 118 89(26) 10− eV s 3:9 10− × × 1=2 8 4 Planck mass (¯hc=G) mP 2:1767(16) 10− kg 7:5 10− 3 1=2 × 35 × 4 Planck length ¯h=mPc = (¯hG=c ) lP 1:6160(12) 10− m 7:5 10− 5 1=2 × 44 × 4 Planck time lP=c = (¯hG=c ) tP 5:3906(40) 10− s 7:5 10− × × ELECTROMAGNETIC 19 8 elementary charge e 1:602 176 462(63) 10− C 3:9 10− × 14 1 × 8 e=h 2:417 989 491(95) 10 AJ− 3:9 10− × × 15 8 magnetic flux quantum h=2e Φ0 2:067 833 636(81) 10− Wb 3:9 10− 2 × 5 × 9 conductance quantum 2e =h G0 7:748 091 696(28) 10− S 3:7 10− 1 × × 9 inverse of conductance quantum G0− 12 906:403 786(47) Ω 3:7 10− a 9 1 × 8 Josephson constant 2e=h KJ 483 597:898(19) 10 Hz V− 3:9 10− von Klitzing constantb × × 2 9 h=e = µ0c=2α RK 25 812:807 572(95) Ω 3:7 10− × 26 1 8 Bohr magneton e¯h=2me µB 927:400 899(37) 10− JT− 4:0 10− 1 × 5 1 × 9 in
    [Show full text]