Spacecraft capture tug
A spacecraft capture tug is disclosed. The tug can capture objects in space, including spacecraft and satellites, using an engagement system and provide propulsion for the object to a point of servicing, repair, or other desired operations. Further, the tug may dock with other specialty tugs to form a custom transport system.
1. A spacecraft capture tug comprising:
a frame having a first and second ends, an outer periphery, and a substantially hollow interior;
a docking adapter disposed on the second end of the frame;
an engagement system disposed on the first end of the frame;
a plurality of chemical tanks disposed within the frame, at least one tank comprised of an oxidizer and one tank comprised of a propellant, each tank having an access valve for refueling in space and each tank removably secured to the frame such that a tank can be replaced in space;
a plurality of nozzles disposed on the outer periphery of the frame and each nozzle having a valve for regulating the flow of the oxidizer and fuel from the tanks, wherein the number and disposition of the nozzles can be chosen for a desired execution of orienting and propelling the tug in space;
a plurality of solar cell arrays disposed on the outer periphery of the frame and each solar cell array having a positioning system such that each array is independently pivotal in relation to the frame;
at least one battery;
a wireless communications system connected to the batteries; and
a computer connected to the at least one battery, the nozzle valves, the positioning system of the solar cell arrays, the solar cell arrays, the communications system, and the computer controls charging of the batteries by the solar cell arrays, directs the flow of the oxidizer and fuel to each nozzle, controls ignition of the oxidizer and fuel combination, controls the positioning of the solar cell arrays, operates the communications system, executes avionics software, provides a status of the tug including the level of oxidizer and fuel in the tanks, operates the docking adapter and the engagement system, and implements a three axis attitude control;
wherein, power is provided to the space tug by the 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 capture other space objects including spacecraft by way of an engagement system and provide propulsion to the captured object.
2. The spacecraft capture tug of claim 1 further comprising a harpoon like gun for attaching a cable like structure between a space object and the space capture tug.