manoftaste
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Both superchargers and turbochargers are basically just air pumps. How much they prevent power loss at altitude depends on how they're designed and controlled (e.g. how much air they can pump at a given altitude vs. engine rpm, and how much they'll pressurize the engine's cylinders before a bypass/waste-gate starts opening.)
My friend, who's a private pilot & flight instructor, reminded me that the British Spitfire was supercharged even back in the 1930s. That's so it would still perform at way over 10,000 feet.
Sure, but I think it had to do with how differently both systems worked. Meaning, Turbocharger operates on the principle of getting the air pressure to reach a certain level by using exhaust, so it may take it a little longer at high altitude to get to the set pressure value due to air being thin, but it eventually will. Vs a Supercharger which is connected to engine itself with a belt/chain and has its spinning mechanism/wheel size designed to reach a certain pressure at sea level. So at higher altitudes that wheel will still be spinning at the same exact speed as at sea level by virtue of its being directly connected to the engine itself, hence producing whatever pressure it can produce using the available air.