Abstract: A method and device for the wireless transmission, in closed spaces, of energy emitted by at least one light source. The energy emitted by the light source is received by at least one solar cell module in the closed space and is converted into electricity. The method includes the steps of reflecting at least a part of the light energy emitted by the light source at a reflective surface inside the space, receiving the reflected light energy in the at least one solar cell module, and converting the reflected light energy into electricity. The device includes at least one solar cell module inside the closed space, configured to receive the light energy and convert the light energy into electricity. At least a portion of the space comprises a reflective inner surface comprising a multilayer insulation surface, at which the energy emitted by at least one light source is reflected.

Abstract: For directly converting heat to electrical energy, for example in a spacecraft operating in space, at least one thermoelectric generator module is arranged in an evacuated chamber so as to receive thermal radiation from a heat source through the interior vacuum within the interior of the chamber. The thermoelectric generator module converts a portion of the received heat to electrical energy and rejects a portion of the heat by thermal conduction to a thermally conducting cooling body such as the chamber wall or directly by thermal radiation to the surrounding vacuum of space.

Abstract: A method and device for the wireless transmission, in closed spaces, of energy emitted by at least one light source. The energy emitted by the light source is received by at least one solar cell module in the closed space and is converted into electricity. The method includes the steps of reflecting at least a part of the light energy emitted by the light source at a reflective surface inside the space, receiving the reflected light energy in the at least one solar cell module, and converting the reflected light energy into electricity. The device includes at least one solar cell module inside the closed space, configured to receive the light energy and convert the light energy into electricity. At least a portion of the space comprises a reflective inner surface comprising a multilayer insulation surface, at which the energy emitted by at least one light source is reflected.

Abstract: For directly converting heat to electrical energy, for example in a spacecraft operating in space, at least one thermoelectric generator module is arranged in an evacuated chamber so as to receive thermal radiation from a heat source through the interior vacuum within the interior of the chamber. The thermoelectric generator module converts a portion of the received heat to electrical energy and rejects a portion of the heat by thermal conduction to a thermally conducting cooling body such as the chamber wall or directly by thermal radiation to the surrounding vacuum of space.