Could an articulated permanent magnet work as a low-power cubesat magnetotorquer? Problems?

Question

Conventional magnetotorquers for cubesats are electromagnets that produce torque in the Earth's magnetic field, and nearly all of the power they use just heats the copper through $\text{I}^2 \text{R}$ losses. A permanent magnet that was articulated with some kind of gimbal-like mechanism that could point it in a wide variety of orientations within the cube could in principle do this as well, using only a tiny fraction of the power.

There are a lot of design issues related to a magnetic design that would maximize the effect while keeping weight down. There might need to be a fail-safe parked position so that the satellite would not be "magnetically active" externally until it was fully deployed and operational - a little bit like those magnetic bases used in machine shops. A realistic design might require some finite torque in the articulation simply due to forces between the magnet and its "safe position" keeper or other ferro-magnetic materials that could be substantially larger than the torque related to the Earth's magnetic field.

1. This sounds great, but is it functionally realistic for a low-U cubesat?
2. Are there rules about permanent magnets inside cubesats - either regulatory or from individual launch providers - that could be a 'deal-breaker'?

below: an example of a Magnetic Base (rotated) from here. The permanent magnet (PM) magnetotorquer would not look like this nor be this heavy. It's just an example of the concept of a PM object with an "off"-like position.

Answer 1

RAX and RAX-2 and possibly other cubesats launched by the University of Michigan (I can't remember at the moment) used fixed neodymium based magnets on their Z+ axis. Hysteresis was added to dump any residual momentum after P-Pod ejection. On the RAX missions, the magnets then were used to orient the satellite vertically over the poles where the science missions were conducted.

I haven't kept close tabs on the smallsat industry lately, but I would estimate that it is totally within the realm of doable, but with its risks. Cubesats are often built out of aluminum. While there may be other ferromagnetic materials used, and current loops in the electronics, I think a well chosen servomotor could over come most issues. The biggest risk in my mind would be dealing with vibration on launch. Moving parts tend to have higher risk.

Yes, there are rules about magnets (and just about everything else) on secondary payloads. The primary payload usually has many times more risk invested so they control almost everything about secondary payloads. The launch provider will have a say as well. It's almost always a case by case basis. The largest risk takers are probably any other secondary payloads on board. For example, M-Cubed (another Michigan launched sat) was believed to have stuck to another cubesat using passive magnetic control, rendering both missions a loss.

Disclaimer: I worked on the missions mentioned here, as well as a few others.