Glazing of Spacecraft

    • 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
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    Parameter Value
    Surface compression stress, Mpa at least 150
    Operation temperature, К 700
    Double refraction nm/cm 40

    Description

    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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