>With most commercial aircrafts using turbofan engines which makes it faster.
Because speed isn’t the only thing to optimize for.
Turboprops are considerably more efficient at slow speeds and lower altitudes. This also makes them capable of taking off from shorter runways.
Also it’s considerably safer to take off from a dirt runway with a turboprop than a turbofan because you don’t have to worry as much about the engine ingesting rocks or whatever.
Those propeller aircraft still have jet engines, they are just connected to a propeller instead of a ducted fan. That gives them different trade-offs, propellers (turboprops) are slower but have better efficiency.
A new type of engine we might see in the next decade or so is an unducted fan engine like the CFM Rise, which aims to combine the efficiency of a turboprop with the speed of a turbofan.
The C-130 is a roughly 70 year old airplane. At the time when it was designed, the large, highly efficient turbofans that power our commercial airliners didn’t yet exist.
Other commenters have pointed out several other good reasons (such as efficiency at low speed/low altitude) to pick turboprop engines for similar roles. The Airbus A400 is a contemporary example. One reason that hasn’t been mentioned yet is that turboprop engines are typically more tolerant of sandy/dusty environments versus turbofans.
For smaller “general aviation” aircraft like a Cessna 172, the reason they’re still propeller-powered is two-fold: jet engines are much more expensive and maintenance intensive than radial/cylinder engines that produce similar amounts of thrust, and small jet engines are also EXTREMELY inefficient for the amount of thrust that they produce.
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