Shortround6
Lieutenant General
Quite true and it turns out that larger, heavier planes can be adapted to lives (roles) better (easier) than smaller aircraft can.If a fighter turned out to be successful, it was going to have lives far beyond what the original planners theorized about.
Also sort of depends on how far the designers are willing to go with it.
I love the Curtiss 75-81-87 from a design history standpoint. I don't believe any fighter (or aircraft?) went through so many different engines or design variations.
All while keeping original wing dimensions and airfoil except for the P-40Q.
There will possibly be some argument from the Spitfire fans.
The Hawk family was on the 4th engine by the time they got to the P-36.
My own engine count is going differ from some others as I am going to only credit the Spitfire with 4 basic engines. Single stage Merlin, two stage Merlin, single stage Griffon and two stage Griffon.
Hawk Family got the turbo Allison (P-37), the single speed/single stage Allison, 1 two stage P&W R-1830, the Merlin and the 2 stage geared Allison in the P-40Q. I am lumping all of the single stage R-1830s and R-1820s together in the first 4 engines regardless of power, supercharger gears.
Obviously some combinations were more successful than others.
Getting back the "light weight" I do not know what the airframe weight of the original Hawk 75 was. We do know that the Fixed gear Hawk 75H
used a 780lb wing. The later P-40s used a wing just over 1100lbs, weight gain of 145kg just in the wing. Partially to address wing strength issues, partially to allow for more armament and partially to accommodate higher gross weight. Change in powerplant from the 9 cylinder cyclone to the Allison used in the early P-40s was over 640lbs. (290kg). So when does the Hawk go from light fighter to standard fighter?
The P-40 (no letter) Gained about 1500lbs over the Hawk 75H but doubled the firepower (two .50s in the cowl with 200rpg and two .30s in the wings with 500rpg).
Very few people are going to say that 6800lb P-40 is a light fighter. The early P-40 carried no protection and no underwing/fuselage load.
Now with aid of history we can see that the Curtiss design was sort of past it's prime in the fall of 1940 (NA-73) but that took a while to realize. The US also didn't want to screw with the production lines as the US Army only had two fighters in large scale production in 1941-42 since the other one was the P-39 things were not looking good.
Dec 1940 production 0 P-38s, 10 P-39s, 165 P-40s
June 1941 production 4 P-38s, 37 P-39s, 125 P-40s (change over from P-40C to P-40D/E
Dec 1941 production 54 P-38s, 191 P-39s, 285 P-40s.
Republic was working on the XP-47 "light fighter"
Using the same engine (?) as the early P-40s and a similar armament. Two .50s to start and four (?) .30s added in the wings later.
Details as to wing size and weight are very sketchy. Initially a 4900lb aircraft with a 115sq ft wing with no wing guns (Aug 1939). With a 2500lb powerplant one wonders how they planned to do that? Rapidly grew to a 6150lb plane with a 165 sq ft wing that did include the wing guns. And we are no longer in the light fighter catagory.
One does wonder how such a plane would have faired in NA or in the Pacific. Fast but without changing the engine/supercharger getting to 20,000ft to fight may have been tricky and range/ground attack would have been not as good. Very French looking though
