Description:The satellite for junk removal, includes a toroid-shaped body designed for stability in space and precise maneuverability, a set of solar panels with monocrystalline solar cells to generate power for the satellite's operations, a lithium-ion battery with a capacity of 50 kWh for storing and supplying power as needed, a reaction control thruster (RCS thrusters) strategically positioned on the toroid body for precise orbital adjustments, chemical thrusters for larger orbital maneuvers, an integrated thermal control system with heaters, radiators, insulation, and a control system to manage the satellite's temperature, a mechanical arm with the capability to capture and deorbit junk satellites, a detachable panel housing a reaction control thruster (RCB thruster) for moving the captured junk satellite into a decaying orbit, and a control system with real-time monitoring and tracking capabilities , Claims:1. A satellite for junk removal, comprising:
a toroid-shaped body designed for stability in space and precise maneuverability;
a set of solar panels with monocrystalline solar cells to generate power for the satellite's operations;
a lithium-ion battery with a capacity of 50 kWh for storing and supplying power as needed;
a reaction control thruster (RCS thrusters) strategically positioned on the toroid body for precise orbital adjustments;
chemical thrusters for larger orbital maneuvers;
an integrated thermal control system with heaters, radiators, insulation, and a control system to manage the satellite's temperature;
a mechanical arm with the capability to capture and deorbit junk satellites;
a detachable panel housing a reaction control thruster (RCB thruster) for moving the captured junk satellite into a decaying orbit; and
a control system with real-time monitoring and tracking capabilities.
2. The satellite for junk removal of claim 1, wherein the toroid-shaped body is constructed from graphene and carbon fiber, providing increased strength, reduced weight, and improved conductivity.
3. The satellite for junk removal of claim 1, further comprising an education module providing users with information on space debris and the satellite's role in mitigating the problem, promoting awareness and understanding of the importance of space debris removal.
4. The satellite for junk removal of claim 1, wherein the satellite is designed to deorbit multiple junk satellites in a single mission, thereby increasing its efficiency and cost-effectiveness.
5. A method for removing space debris using a satellite, comprising:
launching the satellite into orbit;
positioning the satellite to intercept and capture a target junk satellite;
using the mechanical arm to capture the target junk satellite;
transporting the captured junk satellite to a decaying orbit;
releasing the captured junk satellite into the decaying orbit to facilitate its re-entry into Earth's atmosphere; and
repeating the process for additional junk satellites.
6. The method of claim 5, further comprising real-time monitoring and tracking of the space debris removal process, allowing users to observe and learn from the satellite's operations.
7. The method of claim 5, wherein the satellite coordinates the capture and release of junk satellites to maximize efficiency and minimize the risk of collision with other objects in orbit.
8. The method of claim 5, wherein the satellite provides a revocation capability, allowing users to halt the debris removal process or release captured satellites at any stage.
9. The method of claim 5, wherein the satellite is equipped with sensors to detect and avoid collisions with operational satellites and other objects in orbit during the debris removal process.
10. The method of claim 5, further comprising an education module providing users with information on the importance of space debris removal and the ecological impact of reducing debris in Earth's orbit.