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Advanced cryogenic insulation systems are
required to meet future space mission requirements and reduce system mass and
active cooling system power
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Research confirms lack of comprehensive thermo
physical properties of MLI systems
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Emerging technologies and assembly/fabrication
techniques capable of improving MLI performance identified
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Developed fundamental layer-by-layer design and
simulation tool for MLI systems for rapid design and analysis – models seams
and penetrations
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Modeled conduction/radiation down
struts/attachment points
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Developed patented test rig for validating MLI
performance down to liquid hydrogen temperatures with up to 300 layers
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Provides wide range of data for a variety of
cryogenic insulation configurations
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MLI applications:
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Space-based platforms
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Spacecraft
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Launch vehicles, missiles
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Lunar landers
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Stationary and roadable
dewars
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Superconducting devices
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