FIELD: process engineering.
SUBSTANCE: invention relates to production of structural element and may be used, in particular, in space engineering. Proposed method comprises molding unhardened prepreg fabric from composite fibrous material to be hardened at first hardening temperature to preset shape. Said unhardened prepreg fabric is jointed with, at least, one retaining part from composite fibrous material hardened, at least, partially at second hardening temperature. Said unhardened prepreg fabric jointed with said retaining part is hardened at first hardening temperature. Second hardening temperature exceeds first hardening temperature.
EFFECT: simplified process.
12 cl, 6 dwg
