Both my aircraft use two different 12Vdc relays that carry the starting motor cranking current (~500A for the six cylinder 470cu. in. Continental, less for the four cylinder Lycoming).
The first relay is called the
Master Relay. It is mounted near the battery. It carries the cranking current, but is never operated while the starter motor is active, which means it carries the cranking current, but never has to break the circuit while the starter is operating. This means that the coil current is low enough, 1A (12W) so that the relay coil can be energized continuously without overheating. In fact, every electrical load (lighting, avionics, engine instrumentation, flap motor, pitot heat) is supplied through this relay.
The second relay is called the
Starter Relay. It is rated to break the circuit even while its contacts are carrying the full cranking current. This means that the spring that separates the contacts has to have a lot more force to prevent welded contacts. In turn, this requires a coil with a lot more pull-in force to overcome the stronger spring, which raises the coil's power dissipation to the point that the relay can only be operated 15sec out of a 5min period... The starter relay coil current is about 3A (36W).
The Master relay is mounted right on the battery box. The Starter relay is mounted right on the starter motor on the aircraft engine. Those relays are not interchangable.
Those relays look like this: