An object of the present invention is to provide a capture device enabling capture of a target to be captured without direction contact with the target to be captured.

A capture device for capturing a target with a wire includes: a casing that holds a cartridge detachably; and a launch unit that launches a wire stored in the cartridge, the wire having an end portion provided with a weight and another end portion provided with a weight, in which the launch unit launches the wire with a magnetic field generated by a flow of current through a coil.

A magnetic projectile launching system includes an accelerator having a plurality of electromagnets positioned around a circular accelerator pathway. Each electromagnet includes a frame supporting a core having a passageway surrounding the pathway. A conductive coil is wound around an outer surface of the core. A plurality of capacitors are mounted on the frame and electrically connected to the coil. The capacitors are operable to switch from an on-state to an off-state sequentially to form a moving magnetic field which accelerates a projectile around the pathway. At least one of the electromagnets is a movable electromagnet operable to be moved from a first position to a second position. When the movable electromagnet is in the first position, the accelerator is operable to accelerate the projectile around the pathway. When the movable electromagnet is in the second position, the accelerator is operable to launch the projectile tangentially from the pathway.

A series of the relay of the electromagnetic launcher with a gun and a floating launch platform to launch projectiles in space, wherein the projectile is accelerated along a path using electromagnetic force until the projectile reaches a desired direction and position. The direction of the path is determined by orienting the path in the desired direction using a catcher. the catcher and rail gun projectile as high above as possible, coming close to near space. When the said projectile will reach the last platform, it will be launched by the railgun and ignite its rocket engine to take the payload in space or as required to eliminate the need for large rocket boosters to launch the projectile.

In an example, an apparatus includes a cryogenic container configured to store a cryogenic fluid, a superconducting coil disposed within the cryogenic container, and an outer casing surrounding at least a lateral surface area of the cryogenic container. The apparatus is configured such that, while the superconducting coil is carrying a current, is in a superconducting state, and is being cooled by the cryogenic fluid stored in the cryogenic container, an outward magnetic pressure is imposed on the cryogenic container and the outer casing. The cryogenic container and the outer casing are configured to withstand the outward magnetic pressure for at least a predetermined period of time, including while the superconducting coil is being charged to the superconducting state. An occurrence of a trigger event while the outward magnetic pressure is being imposed causes the cryogenic container and the outer casing to expand and burst into radially-dispersed fragments.

In an example, an apparatus includes a cryogenic container configured to store a cryogenic fluid, a superconducting coil disposed within the cryogenic container, and an outer casing surrounding at least a lateral surface area of the cryogenic container. The apparatus is configured such that, while the superconducting coil is carrying a current, is in a superconducting state, and is being cooled by the cryogenic fluid stored in the cryogenic container, an outward magnetic pressure is imposed on the cryogenic container and the outer casing. The cryogenic container and the outer casing are configured to withstand the outward magnetic pressure for at least a predetermined period of time, including while the superconducting coil is being charged to the superconducting state. An occurrence of a trigger event while the outward magnetic pressure is being imposed causes the cryogenic container and the outer casing to expand and burst into radially-dispersed fragments.

A launcher and projectile system include at least one magnet disposed on or within the launcher for charging a wire coil of the projectile to energize the projectile, thereafter having a housing of the projectile rupture, disintegrate, separate or otherwise have an opening created therein after launch to release a payload. In another embodiment, an accessory for a launcher and projectile is provided, the accessory comprising a magnet for charging a projectile that is launched by the launcher. The strength of magnetic field of the magnet may be adjusted for selective performance of the projectile.

A launcher and projectile system include at least one magnet disposed on or within the launcher for charging a wire coil of the projectile to energize the projectile, thereafter having a housing of the projectile rupture, disintegrate, separate or otherwise have an opening created therein after launch to release a payload. In another embodiment, an accessory for a launcher and projectile is provided, the accessory comprising a magnet for charging a projectile that is launched by the launcher. The strength of magnetic field of the magnet may be adjusted for selective performance of the projectile.

A magnetic apparatus and related method and energy product-by-process to motivate linear or rotational motion, comprising: at least one magnet ring tier comprising a ring of a plurality of permanent magnets; a central core comprising a permanent magnet projectile movement channel, an axis of the channel aligned in a direction normal to a geometric plane defined by the magnet ring, and running through a geometric center of the magnet ring; and each of the permanent magnets mounted in the ring at a mount angle thereof, with the components of their polar alignments parallel to the central core all oriented in the same direction; wherein: if the polar alignment of a permanent magnet projectile was introduced with a particular duality-dependent orientation into the permanent magnet projectile movement channel, the magnetic forces between the ring magnets and the projectile would be capable of motivating the permanent magnet projectile relative to the channel.

A magnetic apparatus and related method and energy product-by-process to motivate linear or rotational motion, comprising: at least one magnet ring tier comprising a ring of a plurality of permanent magnets; a central core comprising a permanent magnet projectile movement channel, an axis of the channel aligned in a direction normal to a geometric plane defined by the magnet ring, and running through a geometric center of the magnet ring; and each of the permanent magnets mounted in the ring at a mount angle thereof, with the components of their polar alignments parallel to the central core all oriented in the same direction; wherein: if the polar alignment of a permanent magnet projectile was introduced with a particular duality-dependent orientation into the permanent magnet projectile movement channel, the magnetic forces between the ring magnets and the projectile would be capable of motivating the permanent magnet projectile relative to the channel.

The present subject matter relates to a system and a method for galactic transportation (100). The galactic transportation system (100) may comprise multiple rails (102) arranged in a first direction (103), a platform (108) for supporting a transporter (202), and a control unit (106). Further, the multiple propulsion coils (104) may be arranged in the first direction (103) on one or more of the rails (102). The transporter (202) may further comprise multiple propulsion modules (206). The propulsion coils (104) on the rails (102) may be activated to exert an electromagnetic repulsive force on the propulsion modules (206) of the transporter (202) for propulsion of the transporter (202).