A spin launched unmanned aerial system projectile includes a net means for disabling a selected target. The net means includes deployment mechanism and weights attached thereto which are cast at said target through use of an ejection spring means. Centripetal forces on the still spinning petals/weights open the net means as it is cast at the target.

An entangling projectile for use with a projectile deployment system includes a pair of pellets, at least one of the pair of pellets having a head with a head outer diameter and a shank with a shank outer diameter, the shank outer diameter being less than the head outer diameter. A tether connects the pair of pellets. A shroud is fitted about a shank of the at least one of the pair of pellets, the shroud having a tether opening formed therein to receive the tether, the tether being coupled to the pellet and extending along the shank of the pellet and through the tether opening formed in the shroud.

An entangling projectile for use with a projectile deployment system includes a pair of pellets, at least one of the pair of pellets having a head with a head outer diameter and a shank with a shank outer diameter, the shank outer diameter being less than the head outer diameter. A tether connects the pair of pellets. A shroud is fitted about a shank of the at least one of the pair of pellets, the shroud having a tether opening formed therein to receive the tether, the tether being coupled to the pellet and extending along the shank of the pellet and through the tether opening formed in the shroud.

This disclosure describes various techniques and systems for rapid low-cost access to suborbital and orbital space and accommodation of acceleration of sensitive payloads to space. For example, a distributed gas injection system may be used in a ram accelerator to launch multiple payloads through the atmosphere. Additionally or alternatively, multiple projectiles may assemble during flight through the atmosphere to transfer and/or resources to another projectile.

A projectile deployment system includes an entangling projectile including a pair of pellets and a tether connecting the pellets. A projectile casing includes a pair of sockets, each socket sized to carry one of the pair of pellets and a selectively activatable pressure source, carried by the projectile casing. The pressure source is capable of expelling the entangling projectile from the projectile casing toward a subject. A launcher carries an activator operable to activate the pressure source to expel the entangling projectile from the projectile casing toward the subject. The projectile casing is removably engageable with the launcher to allow removal of the projectile casing from the launcher after expulsion of the entangling projectile from the projectile casing.

A projectile deployment system includes an entangling projectile having a pair of pellets and a tether connecting the pellets. A projectile casing includes a pair of sockets, each socket sized to carry one of the pellets, the sockets being oriented at an acute angle relative to a longitudinal axis of the projectile casing such that the pellets travel apart from one another as they are expelled from the projectile casing. A launcher carries the casing and includes a selectively activatable pressure source capable of expelling the entangling projectile from the projectile casing toward a subject.

A cannon projectile having an elongated body with a plurality of elongated and circumferentially spaced segments. At least one tether is attached to at least one end of the segments to hold the segments together. A deployment device, when activated, enables the segments to deploy radially outwardly into a pattern controlled at least in part by the at least one tether using aerodynamic and inertial forces only.

The present invention discloses a projectile device for the nonlethal immobilization of threats. The invention includes a plurality of grappling-type hooking assemblies attached by a flexible means to a projectile core, a means for the dispersal of the hooking assemblies on or just prior to impact on a target, and a means for ballistically deploying the device from a 12 gauge shotgun, a 35 mm flare gun, a 40 mm grenade launcher, or other suitable launching device. In particular, the hooking assemblies disperse and adhere to the target, while the flexible attachment means entangle and either limit the motion of or immobilize the target.

The present invention surrounds a payload for use as a projectile for disabling and neutralizing Unmanned Aerial Vehicle (UAV) threats and the like. The payload uses a central projectile and one or more satellite projectiles tethered to central projectile. The satellite projectiles provide entangling elements. The satellite projectiles are configured to expand outward from the central projectile after firing to provide an entangling projectile system wherein any object or individual within the entangling zone of the projectile system can be ensnared and neutralized through the entangling action of the projectile system.

The present invention surrounds a payload for use as a projectile for disabling and neutralizing Unmanned Aerial Vehicle (UAV) threats and the like. The payload uses a central projectile and one or more satellite projectiles tethered to central projectile. The satellite projectiles provide entangling elements. The satellite projectiles are configured to expand outward from the central projectile after firing to provide an entangling projectile system wherein any object or individual within the entangling zone of the projectile system can be ensnared and neutralized through the entangling action of the projectile system.