Fairing

    • Fairing

    Purpose:
    Design and manufacture of head fairings for the protection of spacecraft and upper stage from aerodynamic and thermal loads during ILV passage through dense atmospheric layers.
    Flight qualification of the product: Yes
    Brief history of flight qualification:
    HF 1.750 for Soyuz launch vehicle (Ø 3715 mm, length 8450 mm) with upper stage "Fregat". Mass of HF ≈ 1180 kg. HF 14S737 for the Soyuz launch vehicle (Ø 3715 mm, length 10400 mm) with the "Fregat" upper stage. Mass of HF ≈ 1400 kg.
    Possibility to adapt the product to customer requirements: Yes
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    Parameter Value
    HF RBF 1.750 for the Soyuz launch vehicle Ø 3715 mm, length 8450 mm
    HF 14S737 for the Soyuz launch vehicle Ø 3715 mm, length 10400 mm
    HF AMGE, HF 465GK.G for the Zenit launch vehicle Ø 4100 mm, length 10400 mm
    HF AMG for the Zenit launch vehicle Ø 4100 mm, length 11350 mm
    Mass HF, kg 1180/ 1400/ 1670/ 1870

    Description

    In accordance with the specification of the customer.

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