A nosecone apparatus for hypersonic aircraft, rocket or missiles using a method for the mitigation of the created the shock front of a rocket or aerospace plane flying at hypersonic speeds by using nosecone splines to create both centripetal and isentropic airflows in conjunction with regeneratively cooling the nosecone structure.

A nosecone apparatus for hypersonic aircraft, rocket or missiles using a method for the mitigation of the created the shock front of a rocket or aerospace plane flying at hypersonic speeds by using nosecone splines to create both centripetal and isentropic airflows in conjunction with regeneratively cooling the nosecone structure.

A projectile for short firing ranges includes as a cylinder with a nose having a substantially flat surface arranged with a threaded socket allowing for the arrangement of, for example, a fuze a rear section designed with a substantially flat surface, as well as a projectile body arranged with energetic material enclosed by a casing.

A projectile for short firing ranges includes as a cylinder with a nose having a substantially flat surface arranged with a threaded socket allowing for the arrangement of, for example, a fuze a rear section designed with a substantially flat surface, as well as a projectile body arranged with energetic material enclosed by a casing.

The present invention is a toy projectile and launcher system. The lightweight projectile has an exterior surface symmetrically disposed about an imaginary longitudinal axis. The launcher has planar leaves or holding pins, for receiving and holding the projectile. Within the launcher is a spring-loaded element that moves between cocked and released positions. The spring-loaded element contacts a first planar leaf or a first holding pin as the spring-loaded element moves from cocked to released position. Contact with the spring-loaded element causes the leaves or pins to pinch the projectile and launch the projectile into flight in a direction perpendicular to its longitudinal axis. In an alternate embodiment, rotational and linear velocities are imparted to a projectile by action of a ribbon held against the projectile's exterior surface by parallel members. Contact with the spring-loaded element causes the ribbon to translate along the length of said parallel members and into flight.

A system, apparatus and method for mitigating the shock front of a rocket or aerospace plane flying at hypersonic speeds while simultaneously distilling liquid chemical elements regeneratively from the ambient air by means of vortex inversion splines. The splines may additionally be tuned by geometry to function as both centripetal and/or isentropic thrust augmentation attribute and/or double-decker Joule-Thomson refrigeration means. Because of the stochastic stagnation flux that reaches into the absolute zero zone by means of precooling, a splined stochastically switched hypersonic nosecone may be constructively tuned into a complex Carnot refrigeration engine commanding both personal and enterprise liquid Helium distilling means with orders of magnitude efficacy gains over existing methods.

A jewelry display has a ferromagnetic planar substrate having a front surface opposite a back surface. A wall attachment mechanism is attached to the back surface of the ferromagnetic planar substrate. The wall attachment mechanism is configured to attach the ferromagnetic planar substrate to a substantially vertical surface, such a wall. A plurality of jewelry fixtures are configured to be removably attached to the front surface of the ferromagnetic planar substrate. Each jewelry fixture has at least one permanent magnet and a jewelry holding structure. The at least one permanent magnet of each jewelry fixture is magnetically attracted to the ferromagnetic planar substrate. At least one of the plurality of jewelry fixtures is a ring holding structure, a bracelet holding structure, an earring holding structure, a necklace holding structure, a watch holding structure, a bowl structure or a shelf structure.

A jewelry display has a ferromagnetic planar substrate having a front surface opposite a back surface. A wall attachment mechanism is attached to the back surface of the ferromagnetic planar substrate. The wall attachment mechanism is configured to attach the ferromagnetic planar substrate to a substantially vertical surface, such a wall. A plurality of jewelry fixtures are configured to be removably attached to the front surface of the ferromagnetic planar substrate. Each jewelry fixture has at least one permanent magnet and a jewelry holding structure. The at least one permanent magnet of each jewelry fixture is magnetically attracted to the ferromagnetic planar substrate. At least one of the plurality of jewelry fixtures is a ring holding structure, a bracelet holding structure, an earring holding structure, a necklace holding structure, a watch holding structure, a bowl structure or a shelf structure.

A novel enhanced projectile, designed for use with air rifles and sub-sonic applications is disclosed. The enhanced projectile includes an air core that extends the full length of the projectile.

A novel enhanced projectile, designed for use with air rifles and sub-sonic applications is disclosed. The enhanced projectile includes an air core that extends the full length of the projectile.