Thermal-Protection Materials for Spacecraft
- Purpose: Provision of normal thermal conditions on passing the dense atmosphere at landing, antenna assembly thermal protection.
- Year of release: 1977
- Estimated production / delivery time (months): Depending on the volume of an order
- Flight qualification of the product: Yes
- Brief history of flight qualification: Spacecraft Buran.
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| 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) |
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).
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