Thermal-Protection Materials for Spacecraft
Glavkosmos
Nonablative thermal-protection silica-fiber-reinforced materials for coating the reusable spacecraft (TZMK-10(М) and TZMK-25(М), as well as radio engineering-purpose articles (TZMK-14М).
Technical specifications
- Shape
- blocks, shaped molded or custom -made articles
- Operating temperature, ℃
- from -60 to +1100 short-time – up to +1250
- Substrate
- Silica fiber
- Thermal conductivity at (25±5) ℃,W/mK
- up to 0,050 (for TZMK-10М and TZMK-14М) up to 0,070 (for TZMK-25М)
- Density, kg/m3
- 135-160 (for TZMK-10М, TZMK-14М) 230-280 (for TZMK-25М)
About
Nonablative thermal-protection silica-fiber-reinforced materials for coating the reusable spacecraft (TZMK-10(М) and TZMK-25(М), as well as radio engineering-purpose articles (TZMK-14М).
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
