lv3.0-airframe
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Perform EM Testing with the Assembled Flight Computer Module
It's probably a good idea to check how the module, cradle, and OreSat structure effect the radiation pattern of antennas stuck to the side of the cradle cage. Technically #29 will change the geometry a little bit, but it's probably a fine approximation to use the cradle ring. Actually, covering the ends of the module in foil might even be fine, since the bulkheads only have holes that are 1/8" diameter.
This would still be neat to do, but probably isn't necessary since we stuck the Telemetrum in it and it "just worked", but... the fact that we didn't get launch confirmation from the Telemetrum makes me wonder if it actually had problems. What do you think @glennl and @ryanpdx, do we need to leave this issue open?