I haven't seen much power are you dissipating, sorry if I missed that.
Does the package have a thermal pad?
The stuff I've been involved with for space applications is usually plain old FR4, but often we don't use solder mask or silk screen. We generally test in a thermal vacuum chamber extensively and there's a lot of thermal modelling which is dependent on anticipate in orbit parameters such as varying amounts of time in eclipse.
We also often conformally coat boards, and teflon coated wire is used for interconnects.
At the end of the day the thermal design of the board and system as a whole is key, and you are reliant on local heat conduction and radiation to dissipate that heat away, so methods dependent on convection or fluid conduction don't work... as I'm sure you know!
About ten years ago I was involved on a project where the designer of a solar shunt used a mosfet in its linear region to prevent battery overcharging. In the thermal vacuum chamber, there was no solar simulator, the use case for the shunt in vacuum was never tested. The satellite lasted about a day in orbit before the batteries completely depleted, as the mosfet's failure mode is generally to go short, essentially continually shorting the solar array.
I was involved in a retrospective peer review, it turned out that the designer had read the spec sheet, seen that the max junction temperature was 150 deg C, and designed his heatsink around that figure. Now while it worked in the presence of air to convect the heat away, in a vacuum, well, not so much. Designing for a junction temp of that kind of temperature is daft anyway, and thermal cycling over large temperature ranges will cause repeated physical stresses on the part from differences in coeficients of expansion leasing to early failure.
In general, introducing a pressurised module brings its own complications, but I've never been directly involved in a project that resorted to that, however it was common in Russian space craft to do exactly that for thermal and outgassing reasons. ISTR more recently a hard drive was sent into space in a hermitically sealed pressurised box I believe to stop any lubricants evaporating. Mechanical things in a vacuum is hard precisely because of the lubrication problem, but I am sure you've addressed this too in your motors.
So in short I would steer clear of exotic designs and keep it simple, but also pay close attention to any thermal modelling and thermal vac testing that you do, and that it reflects all the real use cases of your device.
But if you let us know a bit more about the amount of power you are trying to dissipate, maybe we can help further.