Abstract: A pneumatic actuator is designed to dispense a predetermined volume of compressed air from a main tank to an outlet of a solenoid valve. The actuator includes a secondary tank designed to contain such predetermined volume of compressed air. The secondary tank is placed in communication with the main tank through a narrow duct having a through-flow section much smaller than that of the outlet of the solenoid valve.

Abstract: A protection device for a rocket launcher includes a cover with a triplet of openings arranged in angularly equidistant positions so as to allow a passage of the rockets housed in two alternating triplets of rocket housings. An actuation means is designed to rotate the cover between a first position in which the triplet of openings is aligned with the first triplet of openings and a second position in which the triplet of openings is aligned with the second triplet of housings.

Abstract: A container for housing and launching sonar buoys of class G (sonobuoy) including a casing partitioned into two portions and automatic and simplified valve means to sequentially eject the buoys from the container.

Abstract: A protection device for a rocket launcher includes a cover with a triplet of openings arranged in angularly equidistant positions so as to allow a passage of the rockets housed in two alternating triplets of rocket housings. An actuation means is designed to rotate the cover between a first position in which the triplet of openings is aligned with the first triplet of openings and a second position in which the triplet of openings is aligned with the second triplet of housings.

Abstract: Mechanism for restraining and releasing an external airborne load through pneumatic ejection wherein the load supports are made hollow so as to form a tank for the compressed air. The load supports consist of monolithic metal bodies made using an additive manufacturing process.

Abstract: A device for the hold-down and controlled release of space satellites installed on launchers and loads installed on space satellites, includes a blocking member made up of segments radially displaceable from a mutually approached retaining position to a mutually spaced-apart release position of a connecting screw. In order to control the radial displacement of the segments between the retaining position and the release position there are provided a rotatable element coaxial with the blocking member, an articulated mechanism which operatively connects the rotatable element with the segments of the blocking member, and linear motors for driving the controlled rotation of the rotatable element and, through the articulated mechanism, the simultaneous displacement of the segments of the blocking member.

Abstract: A device for the hold-down and controlled release of space satellites installed on launchers and loads installed on space satellites, includes a blocking member made up of segments radially displaceable from a mutually approached retaining position to a mutually spaced-apart release position of a connecting screw. In order to control the radial displacement of the segments between the retaining position and the release position there are provided a rotatable element coaxial with the blocking member, an articulated mechanism which operatively connects the rotatable element with the segments of the blocking member, and linear motors for driving the controlled rotation of the rotatable element and, through the articulated mechanism, the simultaneous displacement of the segments of the blocking member.

Abstract: A device for the hold-down and controlled release of space satellites installed on launchers and loads installed on space satellites, includes a blocking member made up of segments radially displaceable from a mutually approached retaining position to a mutually spaced-apart release position of a connecting screw. In order to control the radial displacement of the segments between the retaining position and the release position there are provided a rotatable element coaxial with the blocking member, an articulated mechanism which operatively connects the rotatable element with the segments of the blocking member, and linear motors for driving the controlled rotation of the rotatable element and, through the articulated mechanism, the simultaneous displacement of the segments of the blocking member.

Abstract: A restrain and release mechanism for an externally airborne load, includes at least one stiff support for suspending the load and an elastically deformable adaptive member designed to maintain the load at pressure contact against the support. The adaptive member is a three-dimensional monolithic metallic body obtained using an additive manufacturing method and having a flexural orthotropic behaviour.

Abstract: A container for housing and launching sonar buoys of class G (sonobuoy) including a casing partitioned into two portions and automatic and simplified valve means to sequentially eject the buoys from the container.

Abstract: A piloting section of a solenoid valve is integrated with a valve section and includes a tubular stem having a distal end placed in communication with the atmosphere and axially displaceable by the solenoid from a receded position, in which a shutter of the valve section is kept in a closing condition, to an advanced position corresponding to an opening condition of the shutter. The shutter has a hollow plunger coaxial with a tubular stem and defining an inner thrust chamber in which, in operation, in the receded position of the tubular stem a fluid pressure—which keeps the shutter in closing condition and which is released into the atmosphere—is applied to displace the shutter to the opening condition, through the proximal end of the tubular stem when it is displaced by the solenoid to the advanced position.

Abstract: Pneumatic actuator designed to dispense a predetermined volume of compressed air from a main tank (2) to an outlet (13) of a solenoid valve (4). The actuator comprises a secondary tank designed to contain such predetermined volume of compressed air. The secondary tank is placed in communication with the main tank through a narrow duct (7) having a through-flow section much smaller than that of the outlet (13) of the solenoid valve (4).

Abstract: A piloting section of a solenoid valve is integrated with a valve section and includes a tubular stem having a distal end placed in communication with the atmosphere and axially displaceable by the solenoid from a receded position, in which a shutter of the valve section is kept in a closing condition, to an advanced position corresponding to an opening condition of the shutter. The shutter has a hollow plunger coaxial with a tubular stem and defining an inner thrust chamber in which, in operation, in the receded position of the tubular stem a fluid pressure—which keeps the shutter in closing condition and which is released into the atmosphere—is applied to displace the shutter to the opening condition, through the proximal end of the tubular stem when it is displaced by the solenoid to the advanced position.

Abstract: A container for housing and launching sonobuoy having a diverter and a casing divided into two portions by a cap. The container is configured to make a presence or an absence of the cap selective so as to be adapted to house and launch a single buoy of class A.

Abstract: A restrain and release mechanism for an externally airborne load, includes at least one stiff support for suspending the load and an elastically deformable adaptive member designed to maintain the load at pressure contact against the support. The adaptive member is a three-dimensional monolithic metallic body obtained using an additive manufacturing method and having a flexural orthotropic behaviour.

Abstract: A device for the hold-down and controlled release of space satellites installed on launchers and loads installed on space satellites, includes a blocking member made up of segments radially displaceable from a mutually approached retaining position to a mutually spaced-apart release position of a connecting screw. In order to control the radial displacement of the segments between the retaining position and the release position there are provided a rotatable element coaxial with the blocking member, an articulated mechanism which operatively connects the rotatable element with the segments of the blocking member, and linear motors for driving the controlled rotation of the rotatable element and, through the articulated mechanism, the simultaneous displacement of the segments of the blocking member.

Abstract: A device for the hold-down and controlled release of space satellites installed on launchers and loads installed on space satellites, includes a blocking member made up of segments radially displaceable from a mutually approached retaining position to a mutually spaced-apart release position of a connecting screw. In order to control the radial displacement of the segments between the retaining position and the release position there are provided a rotatable element coaxial with the blocking member, an articulated mechanism which operatively connects the rotatable element with the segments of the blocking member, and linear motors for driving the controlled rotation of the rotatable element and, through the articulated mechanism, the simultaneous displacement of the segments of the blocking member.

Abstract: A device for the hold-down and controlled release of space satellites installed on launchers and loads installed on space satellites, includes a blocking member made up of segments radially displaceable from a mutually approached retaining position to a mutually spaced-apart release position of a connecting screw. In order to control the radial displacement of the segments between the retaining position and the release position there are provided a rotatable element coaxial with the blocking member, an articulated mechanism which operatively connects the rotatable element with the segments of the blocking member, and linear motors for driving the controlled rotation of the rotatable element and, through the articulated mechanism, the simultaneous displacement of the segments of the blocking member.

Abstract: A device for the hold-down and controlled release of space satellites installed on launchers and loads installed on space satellites, includes a blocking member made up of segments radially displaceable from a mutually approached retaining position to a mutually spaced-apart release position of a connecting screw. In order to control the radial displacement of the segments between the retaining position and the release position there are provided a rotatable element coaxial with the blocking member, an articulated mechanism which operatively connects the rotatable element with the segments of the blocking member, and linear motors for driving the controlled rotation of the rotatable element and, through the articulated mechanism, the simultaneous displacement of the segments of the blocking member.

Abstract: A device for the hold-down and controlled release of space satellites installed on launchers and loads installed on space satellites, includes a blocking member made up of segments radially displaceable from a mutually approached retaining position to a mutually spaced-apart release position of a connecting screw. In order to control the radial displacement of the segments between the retaining position and the release position there are provided a rotatable element coaxial with the blocking member, an articulated mechanism which operatively connects the rotatable element with the segments of the blocking member, and linear motors for driving the controlled rotation of the rotatable element and, through the articulated mechanism, the simultaneous displacement of the segments of the blocking member.