Application material system
Satellite MLI Blankets & External Thermal Protection
Prepare low-mass blanket structures with controlled openings, clean edges, low-outgassing fixing, and geometry matched to spacecraft interfaces.
East Far material scope
Relevant East Far products

CryoMLI 102
Low-emissivity MLI for cryogenic storage, transfer, spacecraft thermal control, and superconducting systems.

CryoMLI 302
Open spacer structure for high-vacuum cryogenic systems, superconducting systems, and spacecraft MLI blankets.

CryoTape PI
High-temperature and cryogenic-compatible tape for aerospace, superconducting, and research systems after project review.

CryoTape MAP
Strong-adhesion cryogenic tape for LNG and LH2 material packages, MLI fixing, and external thermal-protection assemblies.

CryoFiG Fabric
Outer protection and reinforcement fabric for cryogenic material packages.
Engineering scope
Key engineering challenges
- Match blanket geometry to appendages and access points
- Control edge details without creating conductive paths
- Preserve cleanliness through cutting, assembly, packaging, and handling
System layers
- 01 Spacecraft surface
Mission-controlled interface with defined cleanliness and attachment points.
- 02 MLI blanket
CryoMLI reflector / spacer layers profile-cut with controlled openings and local density.
- 03 Edges and attachments
CryoTape or customer-specified low-outgassing fixing used only after compatibility review.
- 04 Outer protection
Mission-selected outer layer matched to exposure, handling, grounding, and contamination requirements.
Supporting materials and supply boundaries
East Far Cryo supplies cryogenic insulation materials, related processing, and material-selection support. Equipment and system responsibilities remain with the project owner and equipment designer.
- Spacecraft structure, grounding hardware, fasteners, coatings, and deployment mechanisms are mission-system items.
- Kapton, outer-cover, mesh, venting, and grounding selections must follow customer drawings and qualification records.
- No flight heritage or institutional relationship is implied by a material recommendation.
Parameters needed for quotation
- Cryogenic medium and normal / transient operating temperatures
- Target vacuum level, pump-down method, hold time, and expected residual-gas load
- Equipment geometry, dimensions or surface area, penetrations, and installation access
- Target heat leak or required layer count and any governing acceptance method
- Required delivery form: rolls, slit widths, sewn blankets, profile-cut parts, or installation kits
- Blanket drawings, surface interfaces, venting / grounding details, cleanliness level, and packaging method
Downloads and technical contact
CryoMLI Series Product Brochure
Product structures, specifications, and application notes for CryoMLI materials.
CryoTape Series Product Brochure
Cryogenic tape structures, temperature ranges, and fixing recommendations.
MLI Technical Reference
Engineering reference for MLI material selection, vacuum, heat flux, and layer density.
We will review your application parameters and reply by email with any clarification questions and the next material-selection step.