A design for developing net thrust using the zero point field was proposed here:

http://mtaonline.net/~hheffner/ZPE-CasimirThrust.pdf

This design appears to be impractical. However, if a superfluid is used the density and velocity can be greatly increased, while simultaneously reducing the drive power requirements, except for refrigeration.

With sufficiently advanced nano-technology, the drive cells could each consist of a cavity with a thin disk that rotates half in the cavity and half out. The half of the disk inside the cavity would experience inertial mass reduction, and thus a reduction in centrifugal force. The actual mass changes occur at the entry and exits from the cavity, and thus have no instantaneous effect on the vertical centrifugal forces at that time. Any energy required or obtained entering the cavity due to Casimir forces is offset by the effect of opposite forces upon exiting the cavity.

A device based on cavity inertial mass change should work many orders of magnitude better using the spinning disk nano-technology approach, or possibly a using a superfluid. Both can increase the density and velocity by orders of magnitude, and thus the mass flow by orders of magnitude and the centrifugal force by orders of magnitude cubed.

These options all have the drawback that vast numbers of complex nano- structures need to be manufactured.

There is a superior method available for implementing the principle of applying anisotropic centrifugal force to Casimir cavity influenced inertial masses. This method consists of building up alternate layers of material, thin layers of conducting or super- conducting material, i.e. casimir cavity boundary layer material, while sandwiching between them layers of readily compressible material which is to be used as the inertial mass altering material. The method further consists of accelerating this material in one direction while compressed, and the other direction while not compressed. Compressing reduces the size of the Casimir cavities, thus increasing the effect and reducing the mass of the compressible material sandwiched between the plates.

The compressible material is likely best implemented as a structure of mixed property material, a vacuous (not dense) highly compressible mesh matrix material enclosing layers or pieces of the material that is to actually act as the inertial mass modifying material. For cooling purposes the mesh material might best be permeable to a cooling medium, or at least produce little heat from repeated compression and expansion.

Call the fully constructed material, which consists of layers of Casimir cavities, "thrust material". Having the material, it is then only necessary to compress it while accelerating in one direction, and release the compression when the material accelerates in the other direction. For example, the thrust material can be mounted around the edges of a wheel and compressed by piezo crystal action only when to one direction from the wheel axis. This produces a net force in the opposed direction. Diamond might make a good inertial mass modifying material due to its close packed structure, high electrical insulating properties, and excellent thermal conduction.

A fully solid state design is feasible. This design uses piezo crystals in two axes. The thrust material is compressed in the x axis for inertial mass reduction, and the much larger oscillated motion is produced by piezo action in the y axis. The thrust is developed in the y axis due to the reduced inertial mass on one half of the y axis cycle, caused by compression of the thrust material in the x axis direction during that half of the y axis cycle.

Best regards,

Horace Heffner
http://www.mtaonline.net/~hheffner/




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