D
Derek A. Tidman
Researcher at General Dynamics
Publications - 5
Citations - 159
Derek A. Tidman is an academic researcher from General Dynamics. The author has contributed to research in topics: Projectile & Hydrogen. The author has an hindex of 5, co-authored 5 publications receiving 159 citations.
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Patent
Cartridge containing plasma source for accelerating a projectile
TL;DR: In this article, a high temperature, high pressure plasma jet source is used to accelerate a projectile through a gun barrel bore by using a tube having an interior wall forming a capillary passage to ionize a dielectric to form a plasma.
Patent
High-pressure having plasma flow transverse to plasma discharge particularly for projectile acceleration
TL;DR: In this paper, a projectile is accelerated through a gun barrel by high pressure gas applied to the rear of the projectile in response to a high pressure plasma discharge, and plasma from the discharge flows transversely of the discharge into a chamber through multiple openings in a passage wall.
Patent
Method of and apparatus for generating hydrogen and projectile accelerating apparatus and method incorporating same
TL;DR: In this article, a projectile is accelerated through a barrel by a high pressure hydrogen gas jet that is derived by exothermically reacting water or a water-hydrogen peroxide liquid mixture with metal or a metal hydride.
Patent
Method of and apparatus for deriving a high pressure, high temperature plasma jet with a dielectric capillary
TL;DR: In this article, a pulsed high pressure, supersonic plasma jet for accelerating a projectile through an elongated confined bore is derived from a dielectric structure including a capillary passage having an interior wall surface from which plasma forming material is ablated in response to a discharge voltage applied to first and second electrodes respectively forming a nozzle and plug at opposite ends of the passage.
Patent
Cartridge having high pressure light gas
TL;DR: In this article, a light gas (34) mixture having a low or intermediate molecular weight and a high or low energy density is applied as a high sound speed gas to accelerate the projectile (12) to speeds of above about 2.4 km/sec.