A vapor jet system to continuously jet vapors while suppressing cavitation. One vapor jet system includes a liquid storage part for separately storing two or more kinds of mutually insoluble liquids; a jet orifice; and a jet control part. Jetting the vapors is from a state where pressure in the space storing the vapors in the liquid storage part is higher than the saturated vapor pressure in any of the two or more kinds of liquids. Alternatively, a vapor jet system can include a fluid storage part storing one kind of liquid and at least one kind of inactive gas having a composition different from the liquid; a similar jet orifice; and a similar jet control part. Jetting the vapors and inactive gas(es) is (are) from a state where pressure in a vapor storing space in the fluid storage part is higher than the saturated vapor pressure in the liquid.

An electron acceleration device using thermionic fission cells and an electromagnetic scoop coil for power. A power control junction and electron injector control that feeds free electrons in packets into the acceleration components that consist of a series of induction linac module units, having quadrupole magnet units in series between the induction module units. Has on-board xenon gas for a deep space electron source. At the high speed electrons exit from the device, deflector plates control the exit path of the electrons to direct the course of a craft.

An electron acceleration device using thermionic fission cells and an electromagnetic scoop coil for power. A power control junction and electron injector control that feeds free electrons in packets into the acceleration components that consist of a series of induction linac module units, having quadrupole magnet units in series between the induction module units. Has on-board xenon gas for a deep space electron source. At the high speed electrons exit from the device, deflector plates control the exit path of the electrons to direct the course of a craft.

A centrifugal force propulsion device is disclosed. The device includes an asymmetrical device enclosure, having a first end wider than a second end. The device includes a magnetically charged mass and a rotating electromagnetic field source encircling the asymmetrical device enclosure, where the asymmetrical device enclosure is accelerated to a high revolutions-per-minute, resulting in a force vector in a direction of the first end of the robotic arm assemblies, and interchangeable robotic arm assembly attachment tools attachable to the attachment end for each of the robotic arm assemblies. The device may include a belt-driven centrifugal force propulsion system including a first pulley coupled to a second pulley by a weighted belt, where the first pulley has a first pulley size greater than a second pulley size and a power source coupled to either of the pulleys to generate a net force vector in the direction of the first pulley.

A centrifugal force propulsion device is disclosed. The device includes an asymmetrical device enclosure, having a first end wider than a second end. The device includes a magnetically charged mass and a rotating electromagnetic field source encircling the asymmetrical device enclosure, where the asymmetrical device enclosure is accelerated to a high revolutions-per-minute, resulting in a force vector in a direction of the first end of the robotic arm assemblies, and interchangeable robotic arm assembly attachment tools attachable to the attachment end for each of the robotic arm assemblies. The device may include a belt-driven centrifugal force propulsion system including a first pulley coupled to a second pulley by a weighted belt, where the first pulley has a first pulley size greater than a second pulley size and a power source coupled to either of the pulleys to generate a net force vector in the direction of the first pulley.

A method and system generate lift for a vehicle relative to a planetary body rotating at a rotational speed. The vehicle incorporates two concentric lift rings in a common plane. The lift rings are positioned such that their common plane is approximately perpendicular to a force of gravity on the planetary body. The hit rings are rotated M opposing directions at speeds that are at least 20 times greater than the rotational speed of the planetary body.

A Relative Superluminal Propulsion Drive that allows for the electro-mechanical means by which a vehicle of mass can be accelerated to and maintain a relative velocity greater than the universal constant C (299,792,458 meters/second, the speed of light in a vacuum) between two fixed points in space when measured from a third fixed point in space. The propulsion drive is an array of electro-mechanical antennas positioned on the forward and aft portion of the vehicle and provides for the force of acceleration to the vehicle by lowering the pressure and density of the energy state of the area in front of the vehicle and increasing the pressure and density of the energy state behind the vehicle through the collection and re-distribution of that part of the electro-magnetic spectrum responsible for maintaining the average pressure density of the void energy of space. In addition to providing propulsion the Relative Superluminal Propulsion Drive accounts for and negates the effects of the Newton's Laws of Motion during both the acceleration and deceleration portion of the travel.

Methods, structures, devices and systems are disclosed for fabrication of microtube engines using membrane template electrodeposition. Such nanomotors operate based on bubble-induced propulsion in biological fluids and salt-rich environments. In one aspect, fabricating microengines includes depositing a polymer layer on a membrane template, depositing a conductive metal layer on the polymer layer, and dissolving the membrane template to release the multilayer microtubes.

A replaceable thrust generating structure for an air vehicle, which includes one or more mounts, which are attachable to the air vehicle, and a thrust generating structure attached to each of the one or more mounts, and wherein the thrust generating structure includes an NMSET element.

A replaceable thrust generating structure for an air vehicle, which includes one or more mounts, which are attachable to the air vehicle, and a thrust generating structure attached to each of the one or more mounts, and wherein the thrust generating structure includes an NMSET element.