Does anyone know why we are specifying (section 2) a maximum no-load voltage of 42 volts? That's in the ballpark of a safety threshold of sort, but does anyone know the history of that one? "28" (nominal, usually spec'd to 22 to 34) volts has been a standard avionics voltage forever, for safety reasons, and our more recent satellites run at 70 to save weight, but I am not sure I have ever heard 42.
I am attempting to do a rules change to better integrate the various bits of the rule book, and that will be a Paragraph 2 change, but I keep getting hung up on unrelated strange things. It kind of looks like a copy-and-paste from FAI, but I would interested in the opinions here.
BTW, all you guys flying gas turbines, be sure yours is below 7 lb, 11, ounces of thrust!
Brett