> .Gene Buckle wrote: > > > Avionics power ratings are always available as nominal and max normal > > draw. Electrical systems are designed with a bit of extra capacity to > > deal with power on rush current, etc. > > > > The only time an aircraft author would have to give the the current draw > > any thought at all is if they're also building special avionics and even > > then, they only really need to specify the nominal draw. The only time > > the breakers will pop is either on command from an instructor station or > > via a random systems failure routine. > > But then there is no need to define amperage in the instruments, is there? >
Yes there is. That's where the load definition belongs. The load figure should follow the equipment, not the bus it's connected to. g. _______________________________________________ Flightgear-devel mailing list [EMAIL PROTECTED] http://mail.flightgear.org/mailman/listinfo/flightgear-devel
