Abstract: The application provides a light expander/contractor device and method of using same, the light expander/contractor device comprising: a faceted quartz structure comprising a lateral surface communicating with a light processing surface at one end and communicating with a planar surface at an opposed end; the light processing surface comprising an initial surface extending from the lateral surface substantially parallel to the planar surface and having a distal end spaced from the lateral surface, the light processing surface further comprising multiple levels of facets comprising quartz-air interfaces: each level of facets comprising (a) a proximal facet surface relative to the lateral surface, the proximal facet surface extending away from the initial surface and toward the lateral surface at a 45° angle relative to the initial surface to communicate with (b) a facet planar surface spaced apart from and parallel to the initial surface to communicate with (c) a distal facet surface adjacent and substantially

Abstract: In one embodiment, the application provides a photon engine comprising one or more cylinders comprising: a primary prism and a secondary prism which may or may not comprise a linear switch, the primary prism comprising one or more light beam inlets and multiple internal faces comprising a primary back face, the secondary prism comprising multiple lateral faces and having a secondary back face positioned adjacent to and spaced apart from the primary back face, forming a non-transparent interface between the primary prism and the secondary prism; the primary prism comprising a light expander/contractor device communicating with the light beam inlet, the light expander/contractor device comprising facets adapted to produce a processed light beam by expanding the diameter of a light beam entering from a given direction; an optic switch comprising a piezoelectric actuator operatively coupled with the primary prism and/or the secondary prism and adapted to (a) compress the secondary back face relative to the primar

Abstract: The application provides a commercially feasible method of flying repeated orbital missions using a Space Shuttle Program (SSP) Orbital Vehicle.

Abstract: A space relevator adapted to transition an object between a stationary compartment and a rotating module rotating in a first direction, the relevator comprising: a relevator module comprising a plurality of substantially solid pie-shaped structures separated by a plurality of pie-shaped compartments all positioned around a central axis; a relevator central shaft extending along the central axis; the relevator module being adapted to receive a rotate signal and a stop signal, one or more of the pie-shaped compartments comprising an entry between the stationary compartment and the rotating module when the relevator module receives a stop signal and after the relevator module receives a rotate signal.

Abstract: A relevator adapted to transition an object between a stationary compartment and a rotating module rotating in a first direction, the relevator comprising: a plurality of concentric substantially solid structures separated by a plurality of concentric compartments all concentrically positioned around a central axis; a relevator central shaft extending along the central axis; the relevator being adapted to receive a rotate signal and a stop signal, one or more of the concentric compartments comprising an entry from the stationary compartment in a stop position and an entry into the rotating module in a rotating position.

Abstract: The application provides a space vehicle comprising a payload bay comprising a pressure vessel comprising a passenger bay module adapted to provide and maintain habitable conditions for twenty or more passengers during a mission traveling from earth to space and back to earth, the habitable conditions comprising (a) one or more service galley within the pressure vessel and adapted for access to the passenger bay module, and (b) the pressure vessel comprising a lavatory module physically separated from and rotatably abutting the passenger bay module, the lavatory module comprising an entry structure allowing access from the passenger bay module into the rotatably abutting lavatory module, the lavatory module comprising rotatable components comprising a lavatory component, the rotatable components being adapted to form the entry structure, wherein relative rotation of the rotatable components is adapted to produce sufficient centrifugal force in the lavatory component to maintain fluids in a sink and a toilet.

Abstract: The application provides a Space Shuttle Program (SSP) Orbital vehicle comprising a payload bay comprising a pressure vessel comprising a passenger bay module adapted to provide and maintain habitable conditions for twenty or more passengers during a mission traveling from earth to space and back to earth.

Abstract: The application provides a commercially feasible method of flying repeated orbital missions using a Space Shuttle Program (SSP) Orbital Vehicle.

Abstract: An apparatus and method provided for utilizing radiation pressure provided by a light wave to generate mechanical work. The apparatus includes a containment chamber constructed to contain the propagation of light waves therein along a predetermined reflected light wave path. The apparatus also an optic switch selectively operable in an open mode and a closed mode, wherein the open mode allows a light wave to enter the containment chamber and the closed mode prevents escape of the light wave from the containment chamber. Further, the apparatus has a reflective mirror positioned at one end of the containment chamber. The reflective mirror has a first reflective surface.