Abstract: A hybrid propulsion engine for a satellite that includes a satellite housing and electronics carried by the satellite housing, may include a rechargeable electrical power source carried by the satellite housing. The hybrid propulsion engine may also include a combustible fuel supply carried by the satellite housing, and an engine housing defining a combustion chamber for fuel from the combustible fuel supply. The hybrid propulsion engine may also include an electrical arc heater associated with the combustion chamber and configured to supply additional heat from the rechargeable electrical power source, and an exhaust nozzle downstream from the combustion chamber.

Abstract: An electronic device may include a circuit board, a heat generating component carried by the circuit board, a heat sink body, and a heat transfer assembly between the heat generating component and the heat sink body. The heat transfer assembly may include a flexible, heat conductive layer having a first portion in thermal contact with the heat generating component and a second portion in thermal contact with the heat sink body. The first and second portions are thermally coupled, and a compressible layer is between the first and second portions of the flexible, heat conductive layer.

Abstract: An electronic device may include a circuit board, a heat generating component carried by the circuit board, a heat transfer rail extending along an edge of circuit board and coupled to the heat generating component, a housing covering the circuit board, and a heat transfer clamp between the heat transfer rail and the housing. The heat transfer clamp includes a flexible, heat conductive layer having a first portion in thermal contact with the heat transfer rail and a second portion in thermal contact with the housing. The first and second portions are thermally coupled, and a clamp and a compressible layer thereon extends between the first and second portions of the flexible, heat conductive layer.

Abstract: An electronic device may include a backplane and an electrical connector carried by a front side of the backplane, and a circuit board assembly removably coupled to the electrical connector. Each circuit board assembly may include a circuit board and electronic components carried by the circuit board and generating waste heat, and a cooling fluid arrangement thermally coupled to the electronic components. The electronic device may include a cooling fluid manifold, and a pair of multi-functional tubes that provide alignment, keying, structural rigidity and fluid supply and return capabilities extending between the cooling fluid manifold and the cooling fluid arrangement.

Abstract: An electronic device may include a backplane and an electrical connector carried by a front side of the backplane, and a circuit board assembly removably coupled to the electrical connector. Each circuit board assembly may include a circuit board and electronic components carried by the circuit board and generating waste heat, and a cooling fluid arrangement thermally coupled to the electronic components. The electronic device may include a cooling fluid manifold, and a pair of multi-functional tubes that provide alignment, keying, structural rigidity and fluid supply and return capabilities extending between the cooling fluid manifold and the cooling fluid arrangement.