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A big problem with modern aircraft and their avionics issues is not the individual pieces of equipment, but interface between systems. Different manufacturer's software can't always understand each other and isn't compatible and in R D that's the biggest cause of delay with electronic systems of modern aircraft than any other. Look at the Australian Seasprites as an example, other issues aside, of cramming too much gadgetry into an existing airframe in a misguided aim to produce extraordinary capability where it never previously existed and the result is an unuseable aircraft.
Gimme' a Skyraider with modern avionics, a modern engine of 3,500 HP, and some smart weapons and I'll show you what an attack plane can do! I want the rotary cannons, too! No more rat-tat-tat ... more of a hummmmm ... and target gone. I'd rathre have a turboprop, but if that's out, a piston did just fine in the real beast, so it should do at least as well with a more reliable modern engine.
Perhaps a closer guide to the use of modern materials and technology is the Formula 1 engine. Simplisticly put, in @1970 it produced 400 bhp at 10k rpm. 40 years later it could put out 950 bhp at 20k rpm (rpm was then limited by the rules.).
This suggests that new materials and ignition control only increased the power from 13.33 bhp per litre per 1k rpm to 15.83 per litre per 1k rpm or barely 19%. The bulk of the total power increase came from the increase in rpm. As the late Keith Duckworth used to say; horsepower is the size of the bang multiplied by the number of bangs per minute.
I agree about fuel injection and ECU's to get the most power for your bang as it were.
I wonder if the use of modern materials would give any significant weight loss?
So improving the power to weight ratio.
What do you guys think?
Cheers
John
Oh, maybe a carbon fiber Mustang??? NICE!