Abstract: The invention relates to a device for pressurizing a standardized two-liquid propulsion system of a geostationary satellite comprising a high pressure helium storage unit (10) having at least one helium storage tank, a regulating unit (11) and a pressurizing unit for propellant tanks (17, 18) interconnected by a pressurizing circuit, wherein the regulating unit is an electronic regulating unit comprising at least one electrovalve (51), positioned at a location of the pressurizing circuit and controlled by a processing and control circuit (54), which receives informations from pressure sensors (43, 47, 48) associated with the different tanks, said processing and control circuit permitting a constant pressure pressurization of the propellant tanks (17, 18) by flow lines including a combination of pyrotechnic valves, filter elements and calibrated leak elements during the satellite transfer and placing in position phase and a measurement of the residual propellant quantity during the orbital life phase of the sa

Abstract: The equipment is usable by a person exposed to NBC threats. It has a helmet, a face-cover provided with fastenings for connection to the helmet and with a coupling for a breathing gas feed or ventilation hose. A flexible envelope extends the helmet and the face-cover downwards. For providing sealed connection between the helmet, the face-cover, and the envelope, a hoop is fixed to the helmet in permanent or removable manner. It projects from the base of the helmet forwards. The top edge of the hoop receives the face-cover and the lower edge hoop receives the envelope in sealed manner.