The invention relates to a missile (1) for intercepting alien drones (21), comprising a capturing net (9) and a parachute (18), wherein a plurality of weights (15) are connected to the capturing net (9), wherein the capturing net (9) can be ejected from the missile (1) and the weights (15) can be ejected from the missile (1). The capturing of the alien drone is improved by the fact that the capturing net (9) can be ejected by a first means and the weights (15) can be ejected by a second means, wherein the weights (15) and the capturing net (9) can be ejected at different times from the missile (1).

The invention relates to a missile (1) for intercepting alien drones (21), comprising a capturing net (9) and a parachute (18), wherein a plurality of weights (15) are connected to the capturing net (9), wherein the capturing net (9) can be ejected from the missile (1) and the weights (15) can be ejected from the missile (1). The capturing of the alien drone is improved by the fact that the capturing net (9) can be ejected by a first means and the weights (15) can be ejected by a second means, wherein the weights (15) and the capturing net (9) can be ejected at different times from the missile (1).

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 canister for storing and launching a self-propelled projectile comprises: a) an inner layer comprising an aluminum foil; b) a top layer consisting of an injected thermoplastic polymer; and c) optionally, a primer and/or a topcoat.

A canister for storing and launching a self-propelled projectile comprises: a) an inner layer comprising an aluminum foil; b) a top layer consisting of an injected thermoplastic polymer; and c) optionally, a primer and/or a topcoat.

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.

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.

A projectile launcher includes: a storage and launching tube suitable for receiving a projectile; a breech sealing one end of the tube; a thruster arranged in the tube between the breech and the projectile, comprising a pressurized gas reserve and suitable for applying an ejection force to a projectile; a plug blocking the other end of the tube, having a locked configuration, in which the plug engages the internal wall of the tube so as to close the tube and to keep the projectile in the tube, and an unlocked configuration, in which the plug is free relative to the tube; and a trigger having a retracted resting configuration and a deployed configuration, suitable for triggering, causing the plug to pass from the locked configuration to the unlocked configuration; wherein the trigger is pneumatic and is supplied with pressure by the reserve.

Proposed is a cover structure with a double cover structure and a shooting case of munition having the same. The cover structure with a double cover structure includes: a shooting case main body having an inner space with an open upper side; a cover member seated on the open upper side of the shooting case main body to seal the open upper side; and a cover fixing member coupled to the shooting case main body to fix a position of the cover member, so that the position of the cover member is strongly fixed while simplifying a structure by the double cover structure to increase an internal pressure of the shooting case, thereby increasing a range of munition and maintaining performance of munition.

Proposed is a cover structure with a double cover structure and a shooting case of munition having the same. The cover structure with a double cover structure includes: a shooting case main body having an inner space with an open upper side; a cover member seated on the open upper side of the shooting case main body to seal the open upper side; and a cover fixing member coupled to the shooting case main body to fix a position of the cover member, so that the position of the cover member is strongly fixed while simplifying a structure by the double cover structure to increase an internal pressure of the shooting case, thereby increasing a range of munition and maintaining performance of munition.