Back to results
US 2022/0250730 A1Published application
Ballistic Engine
OwnerHorace James, JR.inventor
Life of this patent
Estimating the term…
Abstract
An inverted rocket nozzle and pump system suspended and immersed within fluid to be ejected vertically, completely enclosed within an aptly shaped depressurized vessel facilitating vertical propulsion by neutralizing resultant downward thrust and weight of said nozzle and pump system, utilizing the reaction force of fluid jets impinging upon ceiling of said enclosing vessel to induce propulsion.
Claims3
Method of propulsion comprising nozzle enclosed and suspended within vessel to eject fluid in direction of sought propulsion, utilizing deflection of said fluid against inner surface of said vessel.
Dependencies are inferred from the claim text.