Cryogenic Thermal Insulation Systems 16th Thermal and Fluids Analysis Workshop Orlando, Florida August 9, 2005
James E. Fesmire Stan D. Augustynowicz Cryogenics Test Laboratory NASA Kennedy Space Center
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Outline
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Introduction Part 1, Materials Part 2, Testing Part 3, Applications Conclusion
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INTRODUCTION
HEAT IS THE ENEMY
Two things about cryogenics
Store a lot of stuff in a small space
Energy density
Use the cold temperature to do something useful
Refrigeration
Space launch and exploration is an energy intensive endeavor; cryogenics is an energy intensive discipline. Aug 2005
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Cryogenics now touches on nearly every aspect of modern society
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Food Health and medicine Energy Transportation Manufacturing Research Aerospace CryoTestLab
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Cryogenics on Earth and in space
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Cryogens must be stored, handled, and transferred in safe and effective ways Cryogenic usage and application is being extended to the rest of the world in the first half this century People working in cryogenics are becoming more and more specialized CryoTestLab
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For progress and efficiency st into the 21 century, high performance thermal insulation systems are needed….
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Energy Efficiency on Earth
Spaceport facilities
Energy integrated launch site
Propulsion + Power + Life Support
Advanced transfer and storage methods Propellants and gases production Novel components and instrumentation New material applications Thermal insulation structures
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Cost-efficient storage and transfer of cryogens CryoTestLab
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Energy Efficiency in Space
Space exploration
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In-space depots Moon base Mars base Other destinations
Mass-efficient storage and transfer of cryogens
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Energy Efficiency for Industry
Industry Hydrogen Transportation Superconducting Power Processes & Applications
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Thermal Insulation Systems
System Integrated Approach Active + Passive Hot Side + Cold Side
Energy and Economics Perspective Performance must justify the cost Save $$ on energy bill
Two Things About Insulation Conserve energy (or mass) Provide control of system
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PART 1 MATERIALS
Background
Historical perspective D’Arsonval in 1887 to Peterson in 1951 WW II to H2 bomb to Apollo
Conventional materials
Perlite to multilayer to foam
Novel materials Aerogels to sol-gel aerogels Composites old and composites new
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Basics about Materials
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Three Basic Forms Bulk Fill Foams Layered Basic Design Factors Definitions: k-value and CVP
Price versus performance R5 or R1500, its your (extreme) choice Overall Efficiency, four basic factors: 1. Thermal conductivity 2. Vacuum level ($$$) 3. System density or weight 4. Cost of labor ($$) and materials ($)
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1. Thermal Conductivity
Material thermal conductivity
Apparent thermal conductivity
k-value Real systems with large temperature differences
Overall k-value for actual field installation
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milliWatt per meter-Kelvin [mW/m-K] R-value per inch [hr-ft2-degF/Btu-in] 1 mW/m-K = R144
koafi Often one order of magnitude (or more!) higher than reported ideal or laboratory k-values CryoTestLab
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Thermal Insulating Performance of Various Materials MLI System at HV LCI System at HV Aerogel Beads at HV LCI System at SV MLI System at SV Aerogel Composite Blanket Polyurethane Foam Fiberglass Cork Oak Board Ice Whale Blubber Concrete Stainless Steel Pure Copper 0.01
0.1
1
10
100
1000
10000
Thermal Conductivity (milliWatt per meter-Kelvin)
100000
1000000
Representative k-values Material and Density Vacuum, polished surfaces
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