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Homogenization and Optimization of Electrodes and Photovoltaic Cells with Periodic Nanoscopic Geometry
Completed
TRL 3 (started at 2, targeting 3)
Description
The purpose of this proposal is to design a completely propellantless spacecraft control system using magnetic actuators. The operational life and cost of a spacecraft is heavily influenced by its mass which makes propellantless spacecraft control systems an attractive alternative. An electrodynamic tether is a long conducting wire on a spacecraft that interacts with the Earth's magnetic field thereby exchanging orbital angular momentum with the Earth's rotational angular momentum. Electrodynamic tethers can either convert orbital energy into electricity or vice versa. Magnetic torque coils are coils placed on a spacecraft such that when current is passed through the coils in the presence of Earth's magnetic field, a torque is generated which causes an exchange of momentum. Magnetic torque coils provide a propellantless torque which can be used to rotate a spacecraft. However, they cannot generate a torque about the axis parallel to the magnetic field meaning that this axis will be uncontrollable. The goal of this proposal is to compensate for the lack of control by investigating a system consisting of both magnetic torque coils and electrodynamic tethers in order to generate a torque about the uncontrolled axis. My work will focus on the dynamics of the combined system as well as control laws to produce desired attitude or orbit changes. This project can benefit many mission types, especially small satellites that launch as secondary payloads. The ability to change orbit and perform any required attitude maneuvers without the use of propellant will be beneficial to any mission.
Benefits
This project can benefit many mission types, especially small satellites that launch as secondary payloads. The ability to change orbit and perform any required attitude maneuvers without the use of propellant will be beneficial to any mission.
Details
| Technology area | Aerospace Power and Energy Storage > Power Generation and Energy Conversion > Photovoltaic Electrical Power |
| Program | Space Technology Research Grants (STRG) |
| Lead organization | Purdue University-Main Campus, West Lafayette, IN |
| Start date | 2011-08-01 |
| End date | 2015-07-31 |
Project contacts
Listed on TechPort itself — the most direct way to ask about this specific project.
How to get involved
This is early/mid-stage (TRL 3) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.