Abstract: The invention relates to a separation system that dispenses a satellite from a launch vehicle along a dispensing axis, with a first ring for mounting to the launch vehicle and a second ring for mounting to the satellite and a deployment means exerting a separating force on the first and the second ring.

Abstract: A laminate with a decorative layer over an electrical functional layer such as a touch sensor panel, which provides for example a touchpad functionality, as well as a production method for it. It is possible for the first time to perform an individualization of prefabricated laminates with functionality such as touch functionality of a touch sensor in an uncomplicated manner. This is achieved by supplementing a functional laminate with a laser protective layer between the electrical functional layer and a decorative layer which can be lasered and written on with simple measures.

Abstract: The invention relates to an electrical plug connector having an outer conductor contact element with a plurality of elastic spring tabs and a dielectric support element. The spring tabs are arranged, with a respective rear end, annularly around the longitudinal axis (L) of the plug connector and are fastened indirectly or directly to an electrical device. It is provided that the spring tabs are supported with a respective front, free end section laterally on the dielectric support element, wherein the dielectric support element is displaceable laterally relative to the electrical device.

Abstract: A release apparatus for releasing a satellite comprises a release plunger that can be preloaded by a release spring and that is held in a preloaded position by two two-armed pivot levers pivotable about a respective pivot axis, wherein each pivot lever can be held against a force of a spring in a holding position by a release element.

Abstract: The invention relates to a separation system that dispenses a satellite from a launch vehicle along a dispensing axis, with a first ring for mounting to the launch vehicle and a second ring for mounting to the satellite and a deployment means exerting a separating force on the first and the second ring.

Abstract: The invention relates to an ejection unit for at least one satellite, in particular a picosatellite, comprising a frame that defines an inner space for receiving the satellite; and a retention device for holding the satellite in the inner space, the retention device being configured such that the satellite is releasable from the retention device.

Abstract: The invention relates to an ejection unit for at least one satellite, in particular a picosatellite, comprising a frame that defines an inner space for receiving the satellite; and a retention device for holding the satellite in the inner space, the retention device being configured such that the satellite is releasable from the retention device.