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
| 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 |
In accordance with the specification of the customer.
Legal information
Please note that this site is for informational purposes only and under no circumstances is not a public offer determined by the provisions of the Part 2 Article 437 of the Civil code of the Russian Federation.
Information on this site may be changed or supplemented.
