A Hydrogen Leak-Tight, Transparent Cryogenic Sample Container for Ultracold-Neutron Transmission Measurements

Total Page:16

File Type:pdf, Size:1020Kb

A Hydrogen Leak-Tight, Transparent Cryogenic Sample Container for Ultracold-Neutron Transmission Measurements A hydrogen leak-tight, transparent cryogenic sample container for ultracold-neutron transmission measurements Stefan Döge1, 2, 3, ∗ and Jürgen Hingerl1, 2 1Institut Laue–Langevin, 71 avenue des Martyrs, F-38042 Grenoble Cedex 9, France 2Physik-Department, Technische Universität München, D-85748 Garching, Germany 3École Doctorale de Physique, Université Grenoble Alpes, F-38402 Saint-Martin-d’Hères, France The improvement of the number of extractable ultracold neutrons (UCNs) from converters based on solid deuterium (sD2) crystals requires a good understanding of UCN transport and how the crystal’s morphology influences its transparency to UCNs. Measurements of the UCN transmission through cryogenic liquids and solids of interest, such as hydrogen (H2) and deuterium (D2), require sample containers with thin, highly polished and optically transparent windows and a well defined sample thickness. One of the most difficult sealing problems is that of light gases like hydrogen and helium at low temperatures against a high vacuum. Here we report on the design of a sample container with two 1 mm thin amorphous silica windows cold-welded to aluminum clamps using indium wire gaskets, in order to form a simple, reusable and hydrogen-tight cryogenic seal. The container meets the above-mentioned requirements and withstands up to 2 bar hydrogen gas pressure against isolation vacuum in the range of 10−5 to 10−7 mbar at temperatures down to 4.5 K. Additionally, photographs of the crystallization process are shown and discussed. Published as: Review of Scientific Instruments 89, 033903 on 6 March 2018 https://doi.org/10.1063/1.4996296. I. INTRODUCTION II. THE NEED FOR AN IMPROVED SAMPLE CONTAINER If one wants to measure the transmission of ultracold The scattering of thermal and cold neutrons from cryo- neutrons through a cryogenic liquid or solid, the windows genic liquids and solids is a well established experimental of the sample container need to be as highly polished as technique. Most of the time, sample containers and their possible (center-line average roughness Ra < 10 Å) in or- neutron beam windows are machined from aluminum der to minimize undesired scattering from surfaces. Ma- alloy, because of its favorable post-irradiation behavior chined, rough-surface aluminum windows are fairly easy (short half-life of 2.5 min of the 28Al isotope, which is to make and have been used in UCN transmission ex- created by 27Al capturing a neutron), low neutron scat- periments before8–11. As our tests with single-side pol- tering and absorption cross section, and easy workabil- ished aluminum windows and unpolished as well as pol- ity. Thermal and cold neutrons have wavelengths of 1 to ished aluminum foils (Ra in the range of a few µm) have 10 Ångström and are therefore practically insensitive to shown, they are not suitable for UCN transmission ex- the aluminum’s neutron-optical potential, material inho- periments because of significant UCN scattering from the mogeneities and surface roughness. vacuum–aluminum and aluminum–sample interfaces due to surface roughness. Slow neutrons – especially ultracold neutrons (UCNs), In addition, thin aluminum windows in the range of with a velocity of only a few meters per second and a 0.15 to 0.3 mm tend to bulge at a pressure difference of wavelength of several hundred Ångström – are, however, about one bar. This results in a poorly defined sample 1 2,3 sensitive to surface roughness , material and magnetic thickness, which translates directly to a large error in the 4 inhomogeneities . Besides that, aluminum windows are scattering cross section. Atchison et al.8,9 used an initial not optically transparent and thus do not allow for an on- sample thickness of 10.0 mm. However, after bulging of line control of the sample. In UCN applications, the ad- the windows, computer simulations suggested an “effec- vantage of the low neutron-optical potential of aluminum tive thickness” of 11.1 mm. Considering the relation of arXiv:1803.10159v2 [physics.ins-det] 12 Jan 2021 (54 neV) is more than offset by the drawbacks that the sample thickness d and the total cross section σtot in the use of this material entails. transmission equation (eq. 1, where I0 is the transmit- ted UCN flux through an empty sample container, and In this article, we present an improved sample con- I(d) is the transmitted UCN flux through a sample of tainer design which addresses the issues of previous sam- thickness d, Nv is the molecular number density of the ple containers and permits reliable UCN transmission sample), one immediately understands the importance of measurements on cryogenic crystals, such as solid deu- a well defined sample thickness. terium (sD2). Measurements of this kind are needed to interpret the performance of operating sD2-based UCN I(d) −N σ d 5–7 = e v tot (1) sources worldwide . I0 2 Besides exhibiting a low surface roughness, sample con- Since the aforementioned suitable materials are com- tainer windows for UCN transmission experiments should monly supplied as flat wafers and it is very difficult to be made from a material with low absorption cross sec- make them into one-piece structures (like a flat window tion to maximize the neutron flux to the sample, and with plus clamp with screw holes) that would fit into our sam- a low neutron-optical potential12,13 to transmit UCNs ple container11, we had to develop a hydrogen-tight seal with an as low as possible energy. All materials are prac- to join the flat wafers and the clamps made from alu- tically impervious to UCNs with a kinetic energy below minum alloy AlMg3 (AA5754). their respective neutron-optical potential. Materials of choice are thus silicon, transparent vitreous silica and synthetic quartz (SiO2; naming convention suggested by III. DESIGN REQUIREMENTS OF THE Laufer14 to clarify the naming variations of quartz15), SAMPLE CONTAINER AND OPTICAL ACCESS and sapphire (Al2O3). The latter three are optically transparent and allow for an observation of the condensa- A thick and therefore mechanically strong glass slab or tion and crystal growth processes in the sample container collar does not present an obstacle in optical applications. along the neutron beam axis. Amorphous silica has the By contrast, in our case the glass windows need to be as unique advantage of not producing small-angle scatter- thin as possible to minimize the absorption of UCNs. 16 ing inside the material . In our sample containers we First we tried 0.5 mm thick vitreous silica windows in used transparent vitreous silica wafers purchased from our sample container, but they imploded in a vacuum Plan Optik AG, Elsoff, Germany. All of the following test at about 800 mbar pressure difference. Same-size reported results were obtained using sample containers windows, but with a thickness of 1.0 mm, withstood a with these wafers. pressure difference of 1 bar and more, and thus became The fact that the surfaces of the silica windows have a our window material of choice. negligible influence on the measured UCN transmission In brief, the design requirements were: is demonstrated by the virtually identical transmissivity through one d = 1.0 mm window and two d = 0.525 mm • highly polished and thin windows (d = 1 mm), the windows (see Fig. 1). If the surfaces had a large im- windows need to be easily removable pact, four vacuum–silica interfaces would transmit sub- • optically transparent windows with a low neutron- stantially less UCNs than two such interfaces. The calcu- optical potential and of high purity (no scattering lated neutron-optical potential12,13,17 of our amorphous length density inhomogeneities in the material) silica windows based on the volumetric mass density pro- 3 vided by the manufacturer (ρ = 2.203 g/cm ), is 90.6 neV • vacuum seal needs to be easily demountable and at room temperature and the same at cryo-temperatures hydrogen-tight down to 4.5 K due to a volume contraction of less than one per mille. • sample thickness needs to be well defined, the same 1 . 0 across the entire sample area, and adjustable over 0 . 9 a wide range within the same sample container 0 . 8 • sample container needs to withstand 2 bar hydro- gen pressure against high vacuum with a maximum n 0 . 7 −3 o i pressure of 10 mbar, preferably in the range of s s 0 . 6 −5 −7 i 10 to 10 mbar, in order for the closed-cycle re- m s 0 . 5 frigerator to work smoothly and to minimize UCN n a r t up-scattering on residual gas molecules. 0 . 4 e v i t 1 x 0 . 5 2 5 m m a m S i O a 2 The foot of the sample container was designed to be l 0 . 3 e 1 x 1 . 0 m m a m S i O R 2 mounted onto the two-stage cold-head of the cryostat 0 . 2 11 2 x 0 . 5 2 5 m m a m S i O 2 described in Döge et al. with a number of modifica- 2 x 1 . 0 m m a m S i O 0 . 1 2 tions: The stainless steel neutron guides facing directly 0 . 0 the sample container were removed. An illumination unit 2 3 4 5 6 7 8 9 1 0 1 1 1 2 1 3 1 4 with nine white LEDs was mounted on one side of the N e u t r o n v e l o c i t y i n m e d i u m [ m / s ] sample container (see Fig. 2). The LED support had a recess for a 50.8 mm double-side polished undoped sil- FIG.
Recommended publications
  • Studies of the Fast and Exotic Ions in Superfluid Helium-4
    Studies of the Fast and Exotic Ions in Superfluid Helium-4 by Wanchun Wei M.Sc., Brown University, 2009 B.Sc., University of Science and Technology of China, 2005 A dissertation submitted in partial fulfillment of the requirements for the Degree of Doctor of Philosophy in the Department of Physics at Brown University PROVIDENCE, RHODE ISLAND MAY 2012 © Copyright 2012 by Wanchun Wei Vita Wanchun Wei was born on February 3, 1983 in Dalian, China. He received his B.Sc. in Applied Physics from University of Science and Technology of China in 2005. In the fall of that same year, he started his graduate studies in the Physics Department of Brown University. He earned his M.Sc. in Physics in 2009, and a second M.Sc. in Applied Mathematics in 2011. The work for this thesis began in the summer of 2007. During this work, he received the Forest Award for excellent work related to experimental apparatus in 2010. iv Acknowledgements In the seven years of my graduate studies at Brown University, it was a great pleasure to work with my advisor, Professor Humphrey Maris. I have learned a lot from his profound insight in physics and brilliant attitude to life. I deeply appreciate all of his invaluable guidance, inspiration, patience and consideration during the course of my studies. Without these, I couldn’t accomplish this work as a student who started from knowing nothing about cryogenics. I would like to express my gratitude to Professor George Seidel for his valuable advice and deep discussions during this entire work and to Professor Robert Lanou for his kindly help.
    [Show full text]
  • Lawrence Berkeley National Laboratory Recent Work
    Lawrence Berkeley National Laboratory Recent Work Title Design and construction of the DEAP-3600 dark matter detector Permalink https://escholarship.org/uc/item/7wv4t38s Authors Amaudruz, PA Baldwin, M Batygov, M et al. Publication Date 2019-03-01 DOI 10.1016/j.astropartphys.2018.09.006 Peer reviewed eScholarship.org Powered by the California Digital Library University of California Design and Construction of the DEAP-3600 Dark Matter Detector P.-A. Amaudruzl, M. Baldwinj, M. Batygovd, B. Beltrana, C. E. Binaa, D. Bishopl, J. Bonattf, G. Boormani, M. G. Boulayf,c, B. Broermanf, T. Bromwichh, J. F. Buenoa, P. M. Burghardtk, A. Butcheri, B. Caif, S. Chanl, M. Chenf, R. Chouinarda, S. Churchwellh, B. T. Clevelandg,d, D. Cranshawf, K. Deringf, J. DiGioseffof, S. Dittmeierl, F. A. Duncany,g,d, M. Dunfordc, A. Erlandsonb,c, N. Fatemighomii, S. Florianf, A. Flowerf, R. J. Fordg,d, R. Gagnonf, P. Giampaf, V. V. Golovkob, P. Gorela,g,d, R. Gorneac, E. Gracei, K. Grahamc, D. R. Granta, E. Gulyevl, A. Halli, A. L. Hallina, M. Hamstraf,c, P. J. Harveyf, C. Hearnsf, C. J. Jillingsg,d, O. Kamaevb, A. Kempi, M. Ku´zniakf,c, S. Langrockd, F. La Ziai, B. Lehnertc, O. Lig, J. J. Lidgardf, P. Liimataineng, C. Liml, T. Lindnerl, Y. Linnl, S. Liua, P. Majewskij, R. Mathewf, A. B. McDonaldf, T. McElroya, K. McFarlaneg, T. McGinny,f, J. B. McLaughlinf, S. Meadl, R. Mehdiyevc, C. Mielnichuka, J. Monroei, A. Muirl, P. Nadeauf, C. Nantaisf, C. Nga, A. J. Noblef, E. O'Dwyerf, C. Ohlmannl, K. Olchanskil, K. S. Olsena, C.
    [Show full text]
  • 1. Vacuum Requirements ______1 2
    INTRODUCTION TO LABORATORY CRYOGENICS By M. N. Jirmanus, Ph.D. Janis Research Company, Inc. 2 Jewel Drive Wilmington, MA 01887 USA Tel: +1 978 657-8750 Fax: +1 978 658-0349 E-mail: [email protected] www.janis.com PREFACE This work is meant for scientists, students and laboratory personnel who have had little or no experience in cryogenics. It concentrates primarily on cryogenic systems that are commercially available for operation between 1.5 K and 300 K (room temperature). For those users who want to design and build their own equipment, or who are interested in a more detailed analysis of cryogenic systems, a number of excellent references are listed at the end of this booklet. The first section discusses the vacuum requirements of laboratory dewars and variable temperature cryostats. This is followed by a section on liquid helium and liquid nitrogen dewars, and another section on variable temperature cryostats. The next section concentrates on superconducting magnets that are combined with variable temperature cryostats for laboratory experiments, requiring relatively large magnetic fields. Section five describes closed cycle refrigerator cryostats that require no liquid cryogens, and the last section concentrates on experimental techniques, thermometry, and automatic temperature control. This last section also includes a few tables that are helpful in estimating heat loads on the cold stage and attached sample. More detailed information and experimental data are available from the references listed at the end of this booklet. The figures (drawings) spread throughout sections 2 through 6, show a variety of dewar and cryostat designs, based primarily on our experience at Janis.
    [Show full text]
  • Iii 1I W T Tia
    o..ch BriefsSP-5021(21) idex 1979 do iiI 1I W t Tia dk- .T ____ 1-4) 1979 P-5O21 (21)' This document is available from the National Technical Information Service (NTIS), Springfield, Virginia 22161, at price code A06 ($6.50. domestic; $13.00 foreign). Order NASA SP:5021(21). INTRODUCTION Tech Briefs are short announcements of new technology derived from the research and development activities of the National Aeronautics and Space Administration. These briefs emphasize information considered likely to be transferrable across industrial, regional, or disciplinary lines and are issued to encourage commercial application. This Index to NASA Tech Briefs contains abstracts and four indexes -- subject, personal author, originating Center, and Tech Brief number -- for 1979 Tech Briefs. Abstract Section The abstract section is divided into nine categories: Electronic Components and Circuits; Electronic Systems; Physical Sciences; Materials; Life Sciences; Mechanics; Machinery; Fabrication Technology; and Mathematics and Information Sciences. Within each category, abstracts are arranged sequentially by Tech Brief number. A typical abstract entry has these elements: TECH BRIEF NUMBER TITLE e B79-10298 LOW-COMMON-MODE DIFFERENTIAL AMPLIFIER INNOVATOR S. MORRISON (Westinghouse Electric Corp.) r—w Apr. 1980 DATE MSC-18201 Vol. 4. No. 3. p. 323 ABSTRACT Outputs of differential amplifier are excellently matched in phase and amplitude over wide range of frequencies. Common ORIGINATING mode feedback loop offsets differences between two signal paths. CENTER NUMBER Possible applications of circuit are in oscilloscopes, integrated circuit logic tester, and other self contained instruments. The originating Center number in each entry includes an alphabetical prefix that identifies the NASA Center where the Tech Brief originated.
    [Show full text]
  • Earthstorablepropellan
    " 22539-600|-RO-00 t SPACESHUTTLESEALMATERIAL AND DESIGN DEVELOPMENT FOR __ EARTHSTORABLEPROPELLANTSYSTEMS ] 97400508] -002 ; "'""'" D .,_-_., ReportNo. 22539-6001-R0-00 :..v.,.- ContractNo. NAS 9-12729 "'-'- DRL No. 8 :_:_C" DRD No. SE-411T ; ,X,. F I N A L R E P 0 R T e i4 SPACE SHUTTLESEAL MATERIALAND DESIGN -. _.,_,. DEVELOPMENTFOR EARTHSTORABLEPROPELLANTSYSTEMS _ Preparedfor ._ _. , NASA JOHNSONHouston,SPACECRAFTTexas CENTER }_ OCTOBER1973 IIN; H. MACKLIS,AssistanMtanager ChemicalPropulsionDepartment i TRW ONI I_A(:I _AIIIK • NIOONOO IIACH • CALIFORNIA _ IiIm 1974005081-003 :_ ' _- FOREWORD _ This programwas conductedby TRW SystemsGroup,RedondoBeach, _'_ California,undercontractto the NASA JohnsonSpacecraftCenter,Houston, •_- Texas The contractnumberwas NAS 9-12729 ..,_:. The NASA programmanagerwas Mr. J. W. Griffin. _:_ Numerousgovernmentand industrysourcesprovidedsupportthrough- ;_.':_ out the program,but particularlyduringthe state-of-the-artinvesti- -._ gation. Acknowledgmentof thesemany sourcesis providedin the _ Appendices. _i" The Air F_rceMaterialsLaboratory,WrightPattersonAir ForceBase, Dayton,Chio, providedapprovaland supporti_tthe use of the AF-E-411 _. and AF-E-124DmaterialsthroughMr. J. K. Sieron. " _ Personnelat TRW Systemsresponsiblefor the conductof the program _ include: Mr. J. W. M_rtinand Mr. J. R. Denson,AppliedChemistry _ Department;of the ChemicalMr. R.PropN.ulPosionrter,Depar_Mr. .F._nt.L. AdministrativeMerrittand Mr.andH. M.technicalElmendorf I._ Desuppartment;portwas Mr.providedH. Macklis,by Dr. AssistantE.
    [Show full text]
  • Report of Contributions
    ICEC/ICMC 2014 Conference Report of Contributions https://indico.cern.ch/e/ICEC25-ICMC2014 ICEC/ICMC 2014 … / Report of Contributions Course 1: Cryo-Coolers Contribution ID: 0 Type: not specified Course 1: Cryo-Coolers Monday, 7 July 2014 11:00 (6 hours) Presenter: DE WAELE, Fons (Eindhoven University of Technology) Session Classification: Monday Courses September 30, 2021 Page 1 ICEC/ICMC 2014 … / Report of Contributions Course 2: Cryostat Design Contribution ID: 1 Type: not specified Course 2: Cryostat Design Monday, 7 July 2014 11:01 (5h 59m) Presenter: WEISAND, John (European Spallation Source) Session Classification: Monday Courses September 30, 2021 Page 2 ICEC/ICMC 2014 … / Report of Contributions Course 3: Superconducting Materi … Contribution ID: 2 Type: not specified Course 3: Superconducting Materials for Power Applications Monday, 7 July 2014 11:02 (5h 55m) Presenter: TIXADOR, Pascal (CNRS - Grenoble) Session Classification: Monday Courses September 30, 2021 Page 3 ICEC/ICMC 2014 … / Report of Contributions Excursion 1 to AmpaCity in Essen … Contribution ID: 3 Type: not specified Excursion 1 to AmpaCity in Essen/Germany (cable project) and High Magnetic Field Laboratory, HMFL - Nijmegen Friday, 11 July 2014 08:00 (10 hours) Session Classification: Technical Visits September 30, 2021 Page 4 ICEC/ICMC 2014 … / Report of Contributions Excursion 2 to Philips Healthcare, … Contribution ID: 4 Type: not specified Excursion 2 to Philips Healthcare, Stirling and Thales - Eindhoven Friday, 11 July 2014 08:00 (10h 45m) Session Classification:
    [Show full text]
  • INTRODUCTION to LABORATORY CRYOGENICS M.N. Jirmanus, Ph.D
    INTRODUCTION TO LABORATORY CRYOGENICS By M.N. Jirmanus, Ph.D. Janis Research Company, Inc. 2 Jewel Drive Wilmington, MA 01887 Tel: (978) 657·8750 Fax: (978) 658·0349 .' Preface This work is meant for scientists, students, and laboratory personnel who have had little or no experience in cryogenics. It concentrates primarily on cryogenic systems that are commercially available for operation between 1.5 K and 300 K (room temperature). For those users who want to design and build their own equipment, or who are interested in a more detailed analysis of cryogenic systems, a number of excellent references are listed at the end of this booklet. The first section discusses the vacuum requirements for laboratory dewars and variable temperature cryostats. This is followed by a section on liquid helium and liquid nitrogen dewars, and another section on variable temperature cryostats. The next section concentrates on superconducting magnets that are combined with variable temperature cryostats for laboratory experiments, requiring relatively large magnetic fields. section five describes closed cycle refrigerator cryostats that require no liquid cryogens, and the last section concentrates on experimental techniques, thermometry, and automatic temperature control. This last section also includes a few tables that are helpful in estimating heat loads on the cold stage and attached sample. More detailed information and experimental data are available from the referencea.listed.at.the end of this section. The figures (drawings) spread throughout sections 2 through 5, show a variety of dewar and cryostat designs, based primarily on our experience at Janis. These designs have evolved over a 30 year period, and represent a typical cross section of laboratory units that can be used for a wide variety of experiments.
    [Show full text]
  • 2020-03-23T11:01:47+00:00Z -L
    https://ntrs.nasa.gov/search.jsp?R=19720013830 2020-03-23T11:01:47+00:00Z -l FOREWORD It is possible that your company's economic growth can be increased through the use of new and improved materials, equipment, and techniques developed by the aerospace industry. The results of the research and development efforts can assist you in ach ieving lower unit costs, an improved competitive position, developing new products, and increasing the profits of your business. By assisting you in realizing these goals, ASA's and SBA's Technology Util ization Programs are helping to apply the results of the aero­ space industry's research and development activities . Thus, the public earns an in creased return on their invest men t in the space effort. Additional technical information on the material presented can be requested by circling the appropriate number on the Reader Service Card which is included in this compilation. Unless otherwise stated, neither ASA nor SBA contemplates any patent action on the technology described. NOTICE This document was prepared under the ponsorship of the ational Aeronau tics and Space Admini tration. Neither the United States Government nor any person acting on behalf of the United States Government assumes any li abi ljty resulting from the use of the information con tajned in this document, or warrants that such use will be free from privately owned rights. For sale by the National Technical Information Service, Springfield, Virginia 22151. $1.00 CONTENTS SECTION 1. SEALING TECHNIQUES Rubber and Alumin a Gasket~ Retain FOR CRYOGENIC FLUIDS Vacuum Seal in Hi gh -Temperature EMF Cell .
    [Show full text]
  • A Hydrogen Leak-Tight, Transparent Cryogenic Sample Container for Ultracold-Neutron Transmission Measurements Stefan Döge, and Jürgen Hingerl
    A hydrogen leak-tight, transparent cryogenic sample container for ultracold-neutron transmission measurements Stefan Döge, and Jürgen Hingerl Citation: Review of Scientific Instruments 89, 033903 (2018); doi: 10.1063/1.4996296 View online: https://doi.org/10.1063/1.4996296 View Table of Contents: http://aip.scitation.org/toc/rsi/89/3 Published by the American Institute of Physics REVIEW OF SCIENTIFIC INSTRUMENTS 89, 033903 (2018) A hydrogen leak-tight, transparent cryogenic sample container for ultracold-neutron transmission measurements Stefan Doge¨ 1,2,3,a) and Jurgen¨ Hingerl1,2 1Institut Laue–Langevin, 71 Avenue des Martyrs, F-38042 Grenoble Cedex 9, France 2Physik-Department, Technische Universitat¨ Munchen,¨ D-85748 Garching, Germany 3Ecole´ Doctorale de Physique, Universite´ Grenoble Alpes, F-38402 Saint-Martin-d’Heres,` France (Received 15 July 2017; accepted 11 February 2018; published online 6 March 2018) The improvement of the number of extractable ultracold neutrons (UCNs) from converters based on solid deuterium (sD2) crystals requires a good understanding of the UCN transport and how the crystal’s morphology influences its transparency to the UCNs. Measurements of the UCN transmission through cryogenic liquids and solids of interest, such as hydrogen (H2) and deuterium (D2), require sample containers with thin, highly polished and optically transparent windows and a well defined sample thickness. One of the most difficult sealing problems is that of light gases like hydrogen and helium at low temperatures against high vacuum. Here we report on the design of a sample container with two 1 mm thin amorphous silica windows cold-welded to aluminum clamps using indium wire gaskets, in order to form a simple, reusable, and hydrogen-tight cryogenic seal.
    [Show full text]
  • 19720013830.Pdf
    -l FOREWORD It is possible that your company's economic growth can be increased through the use of new and improved materials, equipment, and techniques developed by the aerospace industry. The results of the research and development efforts can assist you in ach ieving lower unit costs, an improved competitive position, developing new products, and increasing the profits of your business. By assisting you in realizing these goals, ASA's and SBA's Technology Util ization Programs are helping to apply the results of the aero­ space industry's research and development activities . Thus, the public earns an in creased return on their invest men t in the space effort. Additional technical information on the material presented can be requested by circling the appropriate number on the Reader Service Card which is included in this compilation. Unless otherwise stated, neither ASA nor SBA contemplates any patent action on the technology described. NOTICE This document was prepared under the ponsorship of the ational Aeronau tics and Space Admini tration. Neither the United States Government nor any person acting on behalf of the United States Government assumes any li abi ljty resulting from the use of the information con tajned in this document, or warrants that such use will be free from privately owned rights. For sale by the National Technical Information Service, Springfield, Virginia 22151. $1.00 CONTENTS SECTION 1. SEALING TECHNIQUES Rubber and Alumin a Gasket~ Retain FOR CRYOGENIC FLUIDS Vacuum Seal in Hi gh -Temperature EMF Cell . .... .. ...... 14 Hi gh -Pressure, Low-Temperature Combination Spacer andGasket Electrical Connector Makes Provides Effective Static Seal.
    [Show full text]
  • Electrical Properties of Quench-Condensed Thin Film
    ELECTRICAL PROPERTIES OF QUENCH-CONDENSED THIN FILM A Thesis by KYOUNGJIN LEE Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE August 2007 Major Subject: Physics ELECTRICAL PROPERTIES OF QUENCH-CONDENSED THIN FILM A Thesis by KYOUNGJIN LEE Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Approved by: Chair of Committee, Winfried Teizer Committee Members, Joseph Ross Hong Liang Head of Department, Edward S. Fry August 2007 Major Subject: Physics iii ABSTRACT Electrical Properties of Quench-Condensed Thin Film. (August 2007) Kyoungjin Lee, B.S., Korea Military Academy Chair of Advisory Committee: Dr. Winfried Teizer Electrical properties of thin film have been an issue of interest for a long time and there are many applications in contemporary industry. Interesting characteristics, such as a metal-insulator transition and superconductivity, were investigated and applied to manufacturing of various electrical devices. In this line of study, many experimental techniques have been introduced for precise measurement of the properties of thin film. Quench-condensation is one of the important techniques in the research of thin films. To facilitate this research, we built a quench-condensation apparatus which can be used for a variety of experiments. The apparatus was designed for the fabrication of ultra- thin film and the in-situ measurement at low temperature. The apparatus was shown to operate well for the fabrication of thin films while monitoring the growth in-situ.
    [Show full text]
  • Arxiv:1712.01982V2 [Astro-Ph.IM] 10 Apr 2018
    Design and Construction of the DEAP-3600 Dark Matter Detector P.-A. Amaudruzl, M. Baldwinj, M. Batygovd, B. Beltrana, C. E. Binaa, D. Bishopl, J. Bonattf, G. Boormani, M. G. Boulayf,c, B. Broermanf, T. Bromwichh, J. F. Buenoa, P. M. Burghardtk, A. Butcheri, B. Caif, S. Chanl, M. Chenf, R. Chouinarda, S. Churchwellh, B. T. Clevelandg,d, D. Cranshawf, K. Deringf, J. DiGioseffof, S. Dittmeierl, F. A. Duncany,g,d, M. Dunfordc, A. Erlandsonb,c, N. Fatemighomii, S. Florianf, A. Flowerf, R. J. Fordg,d, R. Gagnonf, P. Giampaf, V. V. Golovkob, P. Gorela,g,d, R. Gorneac, E. Gracei, K. Grahamc, D. R. Granta, E. Gulyevl, A. Halli, A. L. Hallina, M. Hamstraf,c, P. J. Harveyf, C. Hearnsf, C. J. Jillingsg,d, O. Kamaevb, A. Kempi, M. Ku´zniakf,c, S. Langrockd, F. La Ziai, B. Lehnertc, O. Lig, J. J. Lidgardf, P. Liimataineng, C. Liml, T. Lindnerl, Y. Linnl, S. Liua, P. Majewskij, R. Mathewf, A. B. McDonaldf, T. McElroya, K. McFarlaneg, T. McGinny,f, J. B. McLaughlinf, S. Meadl, R. Mehdiyevc, C. Mielnichuka, J. Monroei, A. Muirl, P. Nadeauf, C. Nantaisf, C. Nga, A. J. Noblef, E. O'Dwyerf, C. Ohlmannl, K. Olchanskil, K. S. Olsena, C. Ouelletc, P. Pasuthipf, S. J. M. Peetersh, T. R. Pollmannd,f,k, E. T. Randb, W. Rauf, C. Rethmeierc, F. Reti`erel, N. Seeburni, B. Shawl, K. Singhraol,a, P. Skensvedf, B. Smithl, N. J. T. Smithg,d, T. Sonleyf, J. Soukupa, R. Stainforthc, C. Stonef, V. Stricklandl,c, B. Surb, J. Tanga, J. Taylori, L. Velocef, E.
    [Show full text]