Requirements for Multi-layer Insulation (MLI) in the LCGT Cryostat

Slides:



Advertisements
Similar presentations
Chapter 8 Heat Transfer & Change of Phase
Advertisements

As close to chemistry as we can get
So Far: Conservation of Mass and Energy Pressure Drop in Pipes Flow Measurement Instruments Flow Control (Valves) Types of Pumps and Pump Sizing This Week:
Temperature, Heat, and the First Law of Thermodynamics
Chapter 11 Energy in Thermal Processes. Vocabulary, 3 Kinds of Energy Internal Energy U = Energy of microscopic motion and inter- molucular forces Work.
Energy in Thermal Processes
Physics 101: Lecture 26 Conduction, Convection, Radiation
In the Atmosphere Thermal Energy Transfer. Temperature and Thermal Energy TEMPERATURE - a measure of the average kinetic energy of the individual particles.
Thermal Energy. Objectives 6.1 Compare and contrast the transfer of thermal energy by conduction, convection, and radiation. 6.1 Differentiate between.
Energy in Thermal Processes
THERMAL CONDUCTION LABORATORY Dr. E. Marotta Department of Mechanical Engineering Clemson University Clemson, SC.
Environmental Testing, Design, Analysis for HABs By: Ara Kourchians (arko)
Cornell notes about heat and how heat transfers
GWADW2011 Elba/Italy, 26/May/2011 N. KIMURA Refrigerator and Cryostat Design for LCGT N. KIMURA A, T. SUZUKI A, S. KOIKE B, T. KUME B, T. OHMORI D, K.
FASTRAC Thermal Model Analysis By Millan Diaz-Aguado.
Layers of the Atmosphere SC SC Layers of the Atmosphere The atmosphere is the layer of gases that surrounds the planet and makes conditions.
Methods of Energy Transfer
Ernie Ihloff 21 May 08 Preliminary Heat Shield Design for nEDM.
Nano/Micro Electro-Mechanical Systems (N/MEMS) Osama O. Awadelkarim Jefferson Science Fellow and Science Advisor U. S. Department of State & Professor.
Plenary This PowerPoint file contains the Plenary for this chapter in Physics For You. Most of these slides are paired with a corresponding slide in.
National Aeronautics and Space Administration Thermal Performance Testing of Cryogenic Multilayer Insulation with Silk Net Spacers Wesley.
LCGT Cryogenics Status Report KEK T.Suzuki.
Thermal Physics Modes of Heat Transfer.
So Far: Conservation of Mass and Energy Pressure Drop in Pipes Flow Measurement Instruments Flow Control (Valves) Types of Pumps and Pump Sizing This Week:
National Aeronautics and Space Administration Demonstration of Hybrid Multilayer Insulation for Fixed Thickness Applications 2015 Cryogenic.
Chapter Eleven: Heat 11.1 Heat 11.2 Heat Transfer.
Investigation 9B  Key Question: How is convection responsible for the movement of air through the atmosphere?? Convection in Earth’s Atmosphere.
Weather Review. Air Masses Air Mass – A large body of air through which temperature and moisture are the same. Types 1. Continental – formed over land.
Conduction and convection require the presence of temperature variations in a material medium. Although radiation originates from matter, its.
Additional Notes. What is the total energy of motion in the molecules of a substance? Thermal Energy.
Heat Transfer in the Atmosphere Essential Question: How is heat transferred in the atmosphere?
Heat Transfer Equations. Fouling Layers of dirt, particles, biological growth, etc. effect resistance to heat transfer We cannot predict fouling factors.
Atomic Layer Deposition for Microchannel Plates Jeffrey Elam Argonne National Laboratory September 24, 2009.
Plumbing and Gas, for better optical cryostats Warren Johnson LSU.
Transmission of Heat. Conduction of heat Takes place within certain materials and from one of these materials to another when they are in direct contact.
HEAT TRANSFER-CONDUCTION CONVECTION AND RADIATION.
Thermodynamics – branch of physics concerned with the study of both thermal and mechanical (or dynamical) concepts. Application: Steam Engines in 1800’s.
LCGT f2f meeting/ICRR, 04/Aug./2011 N. KIMURA Status of the Cryogenics Design N. KIMURA A, S. KOIKE B, T. KUME B, T. OHMORI D, Y. SAITO C, Y. SAKAKIBARA.
Thermal Energy Question Review
Progress and Paper report Sept 23, Progress SPP Manuscript was accepted SPP Manuscript was accepted Evaporation of a multilayer coating with low.
GWADW2011 Elba/Italy, 23/May/2011 N. KIMURA and Y. SAKAKIBARA Present Design of LCGT Cryogenic Payload - Status of Cryogenic Design - N. KIMURA*, Y. SAKAKIBARA**,
Experimental study on heat transfer through a few layers of multilayer insulation from 300 K to 4.2 K Zhanguo Zong, Norihito Ohuchi, Kiyosumi Tsuchiya,
MICE Spectrometer Solenoid Recovery Review - December 3-4, Steve Virostek MICE Spectrometer Solenoid Design and Assembly.
Cryogenics for SuperB IR Magnets J. G. Weisend II SLAC National Accelerator Lab.
Chapter 15 Heat Transfer. Second Law of Thermodynamics Heat flows naturally from hot to cold objects. Heat will not flow spontaneously from cold object.
Cryogenic Safety- HSE seminar CERN,
Heat Transfer.
The 3 Types of Heat Transfer
Cryogenic behavior of the cryogenic system
Performance improvement of vapor compression refrigeration cycle
Requirements for Multi-layer Insulation (MLI) in the LCGT Cryostat
From: Modeling Transmission Effects on Multilayer Insulation
Physics 101: Lecture 26 Conduction, Convection, Radiation
Physics 101: Lecture 24 Conduction, Convection+Radiation
Chapter 8 : Natural Convection
-Honors Thesis Defense- In Situ Ellipsometry of Surfaces in an Ultrahigh Vacuum Thin Film Deposition Chamber Joseph Choi Department of Physics and Astronomy,
PES 1000 – Physics in Everyday Life
0th and 1st law of thermodynamics
Lesson 12 CONDUCTION HEAT TRANSFER
Thermal Control Subsystem
אלון קאופמן, M.Sc מהנדס מעבר חום בכיר אלאופ
ATMOSPHERE Science.
High Performance MLI for Cryogenic Hardware
Layers of the Atmosphere
Energy in the Atmosphere
LCGT f2f meeting ICRR Kashiwanoha
Magnetic shielding and thermal shielding
Thermal engineering of optical mirrors for use at cryogenic
Temperature Distribution Study of Composite Germanium Detector
Presentation transcript:

Requirements for Multi-layer Insulation (MLI) in the LCGT Cryostat (1) Low out-gas rate from the MLI (2) Low heat leak through the MLI T. Ohmoti, M. Kimura , Y. Saito, T. Suzuki F2f meeting, 2011/02/05

MLI utilizes quite a lot of aluminized thin polyester films as radiation shields. The polyester film exhausts water vapor, which may dim the optical system of the Laser-Interferometer. The exhaust rate of the water vapor may be reduced much at cryogenic temperature. But it is important to know the general characteristics of out-gas rate at room temperature.

(1) To reduce the total amount of out-gas, Thickness of polyester film must be thin Light Weight MLI Total number of films in MLI must be reduced High Thermal Resistance

Measurement of Out-gas Rate from the Light Weight MLI Test chamber TMP MLI Sample MLI Sample : Kaneka KFP-9B08 Aluminized 9mm polyester film laminated with thin polyester paper Test Apparatus

The measurement is now underway. MLI : Kaneka KFP-9B08 Back ground (SUS Chamber)

Specific weight of One-layer of MLI MLI Sample w [gf / m2] Crinkled type NRC-2 8.2 IHI Dimple : DAM-06 8.5 IHI Dimple : DAM-12 17.6 Kaneka :KFP-9B08 21 Kaneka :KF-9B / KN-20 26.9 Fermilab Tevatron :LHe Transfer Line DAM + Tissue Glass Paper 49.3 Fermilab Tevatron : Dipole magnet DAM + wavy DAM 67.3 Fermilab : SSC Candidate DAM(1 mil) +2-Cerex spunbonded nylon 55.8

Specifications of Candidate MLI : KFP-9B08 ( provided by Tochigi Kaneka Co., Ltd.) Type of MLI Double Aluminized Polyester Film Laminated with Separator Material All Polyester Thickness Specific weight Surface Resistance of Vapor Deposited Aluminum Layer : Rs less than    for each side of DAM Thickness of Aluminum Layer *1 more than 50 nm for each side of DAM Normal Hemispherical Emissivity Less than 0.1 for non-laminated side Less than 0.6 for laminated side *1 : estimated by the aluminum thickness data obtained by the atomic absorption spectroscopy reported by Teikyo University in the International Conference of Cryogenic Engineering, 2010

(2) High Thermal Resistance Heat transfer mechanisms in MLI qt = qr + qc Radiation term qr and Conduction term qc are comparable at good fabrication condition. Conduction term is governed by contact pressure between reflective films at the self-compression state. Radiation term is governed by total number of films. Thin polyester film will reduce the contact pressure. ⇒ Light weight MLI

Measurement of Heat Flux through MLI MLI Sample GM Refrigerator ( 1.5 W at 4K ) Cold Drum (~5K) Calibration Hearter Heat Leak Meter Warm Drum (~80K) MLI Test calorimeter

Important Test Condition Thermal performance of MLI fabricated in the LCGT cryostat must be evaluated by the data obtained in the laboratory. Key test condition is the compressive pressure between adjacent layers of MLI. Compressive pressure can be evaluated by the layer density of MLI The layer density of MLI in LCGT cryostat must estimated. The actual key test condition of MLI in the laboratory is the layer density of MLI.