Spacecraft are developed on Earth, tested, fully assembled and transported in one piece by a launch vehicle to their respective places of operation. Each component must be designed to withstand the high loads of the launch phase. In most cases, in addition to complex test procedures, this leads to an oversized structure of the spacecraft components, because in orbit they experience only a fraction of the stresses they must endure during rocket launch. The maximum take-off mass required for transport with the launch vehicle and the volume of satellites, for example, thus cause high space transport costs. At the same time, space in the rocket is restricted, which limits the design of the spacecraft from the outset. The search is on for processes that expand the possibilities of future space missions, save resources and reduce costs.
