Abstract: Method of manufacturing a product comprising fiber reinforced polymer material, the method comprising the steps of: providing 10 carbon fibers being embedded in a thermosetting resin, heating 20 the thermosetting resin up to its cure temperature by a current flowing through at least a part of said carbon fibers, letting convert 30 the thermosetting resin to a thermoset polymer. The invention is further directed to a device for performing the method and to a composite sandwich panel structure manufactured according to the method.

Abstract: A payload carrier assembly comprises a payload fairing (1) for protecting at least one payload (3) mounted on at least one payload carrier (20) of a launcher (2), comprising at least one separable fairing part (10, 11) that can be arranged on top of the launcher (2) around the payload (3) to be launched, wherein the payload carrier assembly further comprises at least one first transfer element (4), which is in contact with the at least one fairing part (10, 11) and which, in the assembled state, can be in contact with at least the at least one payload (3) and can transfer forces, applied to the at least one payload (3), to the at least one fairing part (10, 11) and vice versa.

Abstract: Method of manufacturing a product comprising fiber reinforced polymer material, the method comprising the steps of: providing 10 carbon fibers being embedded in a thermosetting resin, heating 20 the thermosetting resin up to its cure temperature by a current flowing through at least a part of said carbon fibers, letting convert 30 the thermosetting resin to a thermoset polymer. The invention is further directed to a device for performing the method and to a composite sandwich panel structure manufactured according to the method.