Patent ID: 9284069
Filing Date: 2016-03-15
CPC Classification: B64G

Claim Text:
1. A solar generator tug comprising: a longitudinal frame having a first and second ends and an inside volume that is in communication with space outside of the longitudinal frame, an outer periphery, and a substantially hollow interior; a docking adapter disposed on the first and second ends of the longitudinal frame; a propulsion system comprising fuel, valves, and nozzles for propelling the tug and the nozzles disposed on the outer periphery of the longitudinal frame, the fuel residing within the longitudinal frame and the docking adapters at opposing ends of the longitudinal frame and the fuel in between the docking adapters; an orienting system comprising fuel, valves, and nozzles for orienting the tug and the nozzles disposed on the outer periphery of the longitudinal frame; at least two tug solar cell arrays disposed on the outer periphery of the longitudinal frame for providing power to the solar generator tug; a plurality of generator solar cell arrays connected to the outer periphery of the longitudinal frame and disposed on opposite sides of the outer periphery of the longitudinal frame and each generator solar cell array having a positioning system such that each array is independently pivotal in relation to the longitudinal frame and each generator solar cell array capable of being transitioned from a stowed configuration to a deployed configuration and the generator solar cell arrays capable of generating at least ten times the amount of power generated by the tug solar cell arrays; at least one battery; a wireless communications system connected to the batteries; and a computer connected to the at least one battery, the propulsion system, the orienting system, the positioning system of the generator solar cell arrays, the tug solar cell arrays, the wireless communications system, and the computer controls charging of the batteries by the tug solar cell arrays, directs the operation of the propulsion system and the orienting system, controls the positioning of the generator solar cell arrays, operates the communications system, executes avionics software, provides a status of the tug including the output of the generator solar cell arrays, operates the docking adapters, and implements a three axis attitude control; wherein, power is provided to the tug by the tug solar cell arrays and the computer can be accessed through a wireless communications so that the tug can be moved to a desired location in space and attached by way of a docking adapter to another craft and provide power from the generator solar cell arrays to the craft.