Abstract: A method for assembling devices on a satellite structure is disclosed including attaching the devices to a first face of a plate drilled with a through-hole provided with a fluid connector, on a second face of the plate, depositing a continuous peripheral bead of polymerisable adhesive composition and depositing a plurality of discontinuous and disjointed inner beads of polymerisable adhesive composition, pressing the second face of the plate against a continuous face of the structure, performing suction so as to create a pressure differential between the plate and the structure, at least partially polymerising the polymerisable adhesive compositions so as to form adhesive joints between the plate and the structure, and interrupting the suction.

Abstract: A device for electrical connection intended to connect a super-insulating mattress to a structural panel of a spacecraft, said connection device comprising: a conducting sleeve having an axis extending in a first direction, said sleeve comprising a device for axial fastening of the insulating mattress and a support, a conductive pin suitable for being arranged in said sleeve, an elastic element carried by said support, said elastic element being suitable for exerting a force on the pin in a direction substantially perpendicular to the first direction in order to press the pin against the sleeve. A method for assembling a female portion of a device for electrical connection to a super-insulating mattress, a super-insulating mattress and a spacecraft.

Abstract: A device for electrical connection intended to connect a super-insulating mattress to a structural panel of a spacecraft, said connection device comprising: a conducting sleeve having an axis extending in a first direction, said sleeve comprising a device for axial fastening of the insulating mattress and a support, a conductive pin suitable for being arranged in said sleeve, an elastic element carried by said support, said elastic element being suitable for exerting a force on the pin in a direction substantially perpendicular to the first direction in order to press the pin against the sleeve. A method for assembling a female portion of a device for electrical connection to a super-insulating mattress, a super-insulating mattress and a spacecraft.

Abstract: Device and process for regulating the power of the engines of a rotary wing multi-engine aircraft. The regulating device (1) comprises, in addition to main regulating systems (2, 6) associated with the engines (M1, M2) of the aircraft, auxiliary regulating systems (12, 13) associated with said engines (M1, M2) and means (10, 11) for determining the speeds of rotation of the engines (M1, M2). Each auxiliary regulating system (12, 13) is capable of automatically adjusting the flow rate of fuel in such a way as to slave the speed of rotation of the associated engine, when its main regulating system has failed, to the speed of rotation of the other engine of the aircraft.

Abstract: Device and process for regulating the power of the engines of a rotary wing multi-engine aircraft.