wuzak
Captain
From real-world events, the people at Curtiss generally pissed off Don Berlin (designer) and weren't paying much, if any, attention to fighter developments that were going on around the world. Witness the P-46 and P-53 (nothing much). The P-60 was a good-handling fighter with very-predictably mediocre speed. There wasn't a "winner" that came from Curtiss-Wright after the P-36 / P-40 series or aircraft, including their last try at it with the XF-87 Blackhawk jet. They had the much-later IBM philosophy of thinking they were the Gold standard and their thinking was "right" and everyone should just know that.
The XP-53 was completed as the XP-60.
The XP-53 was based on a P-40 fuselage with the laminar flow wing and the Continental I-1430 engine.
With the Packard V-1650-1 entering production, the USAAC was keen to combine that engine with the laminar flow wing of teh XP-53. So Curtiss proposed to convert the 2nd XP-53 airframe to the V-1650-1 engine. This would be designated XP-60.
When it was clear the I-1430 wasn't going to be ready for some time, the XP-53 was cancelled.
As Packard was just getting into V-1650-1 production, none were available for the XP-60 to start with, so a Merlin 28 was put in its place instead.The performance was not up to expectations (387mph top speed), so the project did not reach production.
XP-60A and XP-60B were to be V-1710 powered, each with a turbocharger - the A had the GE B series and the B had a Wright turbo.
The XP-60A was built, but had problems with the engine installation (it caught fire in ground running).
The XP-60B was under construction when testing of the XP-60A proved disappointing. The XP-60B was fitted with an R-2800 and single rotation propeller and designated XP-60E. Estimated top speed was about 405mph.
The XP-60C was originally to use the Chrysler IV-2220, but was built with an R-2800 and contra-props.
The XP-60D was the XP-60 fitted with the V-1650-3. I haven't seen any performance numbers for that model.