Abstract: Process for making radomes for the aircraft industry from fabrics and the like of varying weaves, saturated with resins, and allowed to harden in a two-part mold that corresponds to the radome profile, while applying pressure and heat. A stocking-shaped webbing, constituting an outer layer, is inserted into the negative half of the mold, followed by the insertion of a molding material into the so equipped mold half, the material preferably consisting of two components, a resin and fiber clippings various optional steps are suggested by the invention.