CryoMLI 102 CryoMLI cryogenic material product

CryoMLI

CryoMLIFor a qualified evacuated insulation space. Final pressure, pump-down method, residual-gas load, hold time, and vacuum-maintenance strategy must be defined for the installed assembly; performance degrades as gas conduction increases.4K-393K

CryoMLI 102

Low-emissivity MLI for cryogenic storage, transfer, spacecraft thermal control, and superconducting systems.

Typical applicationsCryogenic storage / 4K magnets / Rocket thermal control / Satellite MLI / Deep cryogenic missions

Engineering datasheet

Selection data and declared limitations

Technical sales will review the requested product and application conditions, then reply by email with document availability and next steps.

CryoMLI 102 structure diagram
Structure
Double-sided aluminized PET + fiberglass paper
Temperature range
4 K-393 K
Recommended vacuum condition
For a qualified evacuated insulation space. Final pressure, pump-down method, residual-gas load, hold time, and vacuum-maintenance strategy must be defined for the installed assembly; performance degrades as gas conduction increases.
Thermal performance
Apparent thermal conductivity and heat flux are installed-system values, not unconditional roll-material properties. No single value is published here. Request data for stated hot / cold boundary temperatures, vacuum level, layer density, seam design, and test method.
Width and roll options
Master-roll availability plus custom slitting and rewinding are confirmed by RFQ. Specify finished width, width tolerance, roll length, core, winding direction, and packaging limits.
Layer configuration options
Available as constituent reflector / spacer materials or as project-specific multilayer packages. Layer count and installed density are selected from boundary temperatures, vacuum, geometry, and target heat leak.
Processing options
  • Slitting and rewinding to confirmed dimensions
  • Sewing and blanket assembly where the structure permits
  • Drawing-based or sample-based cutting
  • CNC vibration-knife profile cutting, openings, and project kit packaging
Typical applications
Notes and limitations
  • Not a structural support, pressure boundary, seal, or substitute for vacuum-system design.
  • Published temperature ranges describe constituent material capability; adhesive, seam, contamination, oxygen-service, and installation limits can narrow the usable range.
  • System heat leak must be validated for the actual assembly and test conditions.
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CryoMLI Series Product Brochure

Product technical table

CryoMLI 102 technical data

The table below is published as product-level reference data. Final use still depends on application geometry, vacuum condition, installation density, cleanliness, and customer validation.

ItemUnitTechnical specification
Fiberglass paper basis weightg/m²13 ±0.5
Fiberglass paper thicknessmm0.06 ±0.01
Fiberglass paper moisture content%< 0.2
Fiberglass paper loss on ignition%< 0.2
Fiberglass paper thermal conductivityW/(m·K)< 0.029
Fiberglass paper outgassing ratePa·m³/(s·g)< 1.0×10 -8
Double-sided Aluminized PET (Mylar) basis weightg/m²17 ±1
Double-sided Aluminized PET (Mylar) thicknessmm0.012
Double-sided Aluminized PET (Mylar) coatingÅ600Å+600Å
Double-sided Aluminized PET (Mylar) emissivityε0.014 (@87K, NASA GRC)
Thermal shrinkage rate (180°C, 30min)%≤ 3.0
Spacer Gas Permeability-Moderate (paper barrier, slower pump-down)
Comprehensive tensile strengthMPa≥ 190
Apparent thermal conductivityW/(m·K)< 8.0×10 -5
Reference Heat Flux (40 layers, 78K-294K)W/m²0.66 (ref: NASA A126, DAM + paper)
Operating Vacuum Requirement-< 1×10 -4 Torr (high vacuum) for rated performance
Standard Widthsmm90 / 100 / 200 / 300 / 910 / 1310 / 1800
Maximum Production Widthmm1800
Custom Width-Available (MOQ and surcharge apply)
Composite Layer Configurations-5/5, 10/10, 20/20 (mature); custom available
Recommended Layer Densitylayers/mm1.5 - 2.5
Roll Material — Max Layers-Up to 10/10
Shape Customization-Supported (vibration knife cutting)
Processing Capabilities-Rewinding, sewing, cutting, lamination
Production Method-Fully automated mechanical production
Application Temperature Range-4K(-269°C) - 393K(120°C)
Thermal Shock Resistance-Up to 423K(150°C)