Abstract: The present disclosure relates to a self-contained, random scattering laser generating device comprising a housing comprises an opening and an inner chamber, at least one quantum dot positioned inside the inner chamber, a high-energy emitting source positioned within the inner chamber and in radioactive communication with the at least one quantum dot, and a first lasing medium. The present disclosure also relates to a method comprising providing at least one quantum dot, contacting the at least one quantum dot with a high-energy emitting source whereby randomly scattered light is produced, partially coherently amplifying the randomly scattered light emitted from the at least one quantum dot, and generating a random scattering laser.

Abstract: The present disclosure relates to a light modulating communication device comprising a housing comprising at least one inner chamber, and an opening, at least one quantum dot positioned inside the at least one inner chamber, a high-energy emitting source positioned within the at least one inner chamber, a modulator positioned proximal to the opening of the housing, and optionally, at least one reflector positioned within the at least one inner chamber. The present disclosure also relates to a method comprising providing at least one quantum dot, contacting the at least one quantum dot with high-energy particles such that light is produced from the at least one quantum dot, and modulating the light produced from the at least one quantum dot.

Abstract: The present disclosure relates to illumination devices and methods of generating light for extended periods of time without requiring an outside source of power, recharging, refueling or maintenance. The devices of the present disclosure comprise a plurality of quantum dots and a radioisotope, and may be used in numerous ways, for example, for the marking critical areas or paths, for the illumination of pathways in aircraft, ships, trains, buildings, and other facilities where these routes must be precisely delineated or identified for safety reasons, for the inclusion of signs or other indicia that must be illuminated at all times, as well as many military uses, such as for the demarcation of temporary airfields for fixed-wing aircraft or helicopters or for IFF (identification friend or foe).

Abstract: The present disclosure relates to illumination devices and methods of generating light for extended periods of time without requiring an outside source of power, recharging, refueling or maintenance. The devices of the present disclosure comprise a plurality of quantum dots and a radioisotope, and may be used in numerous ways, for example, for the marking critical areas or paths, for the illumination of pathways in aircraft, ships, trains, buildings, and other facilities where these routes must be precisely delineated or identified for safety reasons, for the inclusion of signs or other indicia that must be illuminated at all times, as well as many military uses, such as for the demarcation of temporary airfields for fixed-wing aircraft or helicopters or for IFF (identification friend or foe).

Abstract: A surveying device and a method for surveying a satellite and its environs is disclosed. The surveying device comprises a docking platform having an interface for physically coupling to a surface of a bus of a spacecraft and an imaging module, releasably coupleable to the docking platform via a semi-rigid tether axially extendable and retractable by command, the imaging module having an imaging sensor for collecting image data, the imaging sensor communicatively coupled with the docking platform via the tether.

Abstract: A surveying device and a method for surveying a satellite and its environs is disclosed. The surveying device comprises a docking platform having an interface for physically coupling to a surface of a bus of a spacecraft and an imaging module, releasably coupleable to the docking platform via a semi-rigid tether axially extendable and retractable by command, the imaging module having an imaging sensor for collecting image data, the imaging sensor communicatively coupled with the docking platform via the tether.

Abstract: The present disclosure relates to a self-powered, random scattering laser generating device comprising a housing comprises an opening and an inner chamber, at least one quantum dot positioned inside the inner chamber, a high-energy emitting source positioned within the inner chamber and in radioactive communication with the at least one quantum dot, and a first lasing medium. The present disclosure also relates to a method comprising providing at least one quantum dot, contacting the at least one quantum dot with a high-energy emitting source whereby randomly scattered light is produced, partially coherently amplifying the randomly scattered light emitted from the at least one quantum dot, and generating a random scattering laser.

Abstract: The present disclosure relates to a light modulating communication device comprising a housing comprising at least one inner chamber, and an opening, at least one quantum dot positioned inside the at least one inner chamber, a high-energy emitting source positioned within the at least one inner chamber, a modulator positioned proximal to the opening of the housing, and optionally, at least one reflector positioned within the at least one inner chamber. The present disclosure also relates to a method comprising providing at least one quantum dot, contacting the at least one quantum dot with high-energy particles such that light is produced from the at least one quantum dot, and modulating the light produced from the at least one quantum dot.

Abstract: A reusable flyback satellite system comprises a refly apparatus and accelerating and positioning apparatus. The refly apparatus provides acceleration and injection into orbit, on-orbit functions services for supporting a payload, de-orbiting, re-entering and landing on a runway. The accelerating and positioning apparatus is attached to a carrier aircraft, the accelerating and positioning apparatus releaseably supporting the refly apparatus. The carrier aircraft positions the accelerating and positioning apparatus at a desired first position wherein the accelerating and positioning apparatus is detached from the carrier aircraft. Thereafter, the accelerating and positioning apparatus positions the refly apparatus to a second position wherein the refly apparatus is detachable from the accelerating and positioning apparatus. The second position is such that the refly apparatus can achieve a desired orbit.