Glazing of Spacecraft
- Purpose: Cockpit glazing (double-chamber structure). Primary glass must withstand the difference between the air pressure in the cockpit and space vacuum.
- Year of release: 1979
- Guaranteed service life (years): at least 15 years
- Estimated production / delivery time (months): 2-3
- Flight qualification of the product: Yes
- Brief history of flight qualification: Buran spacecraft.
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Surface compression stress, Mpa | at least 150 |
| Operation temperature, К | 700 |
| Double refraction nm/cm | 40 |
Heat-resistant high-strength radiation-optically-resistant glass of optical quality for glazing the cabin of the spaceship "Buran". There is a possibility to adapt the product to customer requirements.
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