Abstract: A link device comprising a first object and a second object comprises a first strip, capable of passing from a configuration wound about an axis Z about a support fixed to the first object to a configuration deployed along an axis X substantially at right angles to the axis Z, the strip having an end intended to come into contact with the second object, so as to link the first object to the second object.

Abstract: A system for manipulating a space object in space comprises an articulated structure, wherein the articulated structure comprises a single actuator configured to control, equally, the deployment of the structure in space, the gripping of the space object and the folding down of the articulated structure. Developments describe the use of a fixed supporting structure, a threaded rod, a tapped whorl guided by the threaded rod and a set of articulated bars held by pivot links at their interfaces on the tapped whorl and on the fixed supporting structure. Various mechanical configurations are described, notably gripping devices comprising rollers for locking and/or unlocking the space object by separation of the articulated bars. A method of regulation, of control and of adjustment of the manipulation is provided.

Abstract: A projectile extending along an axis X between two ends, the projectile being positioned in a barrel of substantially cylindrical shape of axis X is provided. The projectile comprises: a hollow part at its center, opening onto a first of the two ends of the projectile to receive a compressed fluid, a plurality of vents passing through the projectile from the hollow part substantially perpendicular to the axis X and with a substantially radial outlet to expel the compressed fluid substantially at a tangent to the projectile. The invention also relates to the barrel and to a launch device comprising a projectile and a barrel.

Abstract: A link device comprising a first object and a second object comprises a first strip, capable of passing from a configuration wound about an axis Z about a support fixed to the first object to a configuration deployed along an axis X substantially at right angles to the axis Z, the strip having an end intended to come into contact with the second object, so as to link the first object to the second object.

Abstract: A device for launching using compressed fluid, comprises: a projectile, a barrel having two ends, the projectile being positioned inside the barrel, a first of the two ends allowing the compressed fluid to enter the barrel, a second of the two ends allowing the projectile to leave, a reservoir of compressed fluid connected to the first of the two ends of the barrel. A connecting device comprises a first tape, able to make the transition from a configuration in which it is wound about an axis Z around a support to a configuration in which it is deployed along an axis X substantially perpendicular to the axis Z, the tape having an end fixed to the projectile, and wherein the support is fixed in the barrel.

Abstract: A device for launching using compressed fluid, comprises: a projectile, a barrel having two ends, the projectile being positioned inside the barrel, a first of the two ends allowing the compressed fluid to enter the barrel, a second of the two ends allowing the projectile to leave, a reservoir of compressed fluid connected to the first of the two ends of the barrel. A connecting device comprises a first tape, able to make the transition from a configuration in which it is wound about an axis Z around a support to a configuration in which it is deployed along an axis X substantially perpendicular to the axis Z, the tape having an end fixed to the projectile, and wherein the support is fixed in the barrel.

Abstract: A projectile extending along an axis X between two ends, the projectile being positioned in a barrel of substantially cylindrical shape of axis X is provided. The projectile comprises: a hollow part at its centre, opening onto a first of the two ends of the projectile to receive a compressed fluid, a plurality of vents passing through the projectile from the hollow part substantially perpendicular to the axis X and with a substantially radial outlet to expel the compressed fluid substantially at a tangent to the projectile. The invention also relates to the barrel and to a launch device comprising a projectile and a barrel.

Abstract: A system for manipulating a space object in space comprises an articulated structure, wherein the articulated structure comprises a single actuator configured to control, equally, the deployment of the structure in space, the gripping of the space object and the folding down of the articulated structure. Developments describe the use of a fixed supporting structure, a threaded rod, a tapped whorl guided by the threaded rod and a set of articulated bars held by pivot links at their interfaces on the tapped whorl and on the fixed supporting structure. Various mechanical configurations are described, notably gripping devices comprising rollers for locking and/or unlocking the space object by separation of the articulated bars. A method of regulation, of control and of adjustment of the manipulation is provided.