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IIRC the P-51 pilots were to take off on fuselage tank (85 USG), expand a half of it, then switch to external fuel? That would leave some 40-45 USG (or 32-35 imp gals) prior using the drop tanks.
I agree that it would be very hard* to make a P-51 from a Spit (range-wise), but a Spit VIII with 30 imp gals in the rear fus. tank would be very close. And feasible/available in early 1943, the best quality of the modification had it been done.
*but not impossible, see Yak-9D/DD
...
Typhoon ... We need to find the way to install another, say, 40 IG into the plane. In wing leading edge, perhaps - all the way from fuselage to cannons.
Every 5 min on combat power subtracts 75 or 60 miles. So 3 x 5 min on combat power makes the 'return range' of 385 or 310 miles.
Was there a way to 'sneak in' the F4U-1 in the ETO as a long range fighter? Maybe under RAF's guise?
At 21500 ft and with 360 gals of internal fuel, the endurance was 5 hrs 20 mins at 75% of the high speed - 1600 miles?
The plane carried 237 gallons in a protected fuselage tank. Each wing had a 57 gallon tank, unprotected, but with a CO2 system to keep fuel vapors from reaching a flammable range. Very early planes carried NO drop tanks. Later planes deleted the wing tanks and adopted two drop tanks instead of one.
that i think is going to be the determining "straw for the camel"...you can load up a lot of planes with external tanks and get them long distances you want....but once they drop their tanks they have to be able to engage in combat and still make it all the way home on their inboard fuel...so you are back to your original configurations and possible in frame mods.
We need to find the way to install another, say, 40 IG into the plane.
Well than - maybe an L-shaped tank, a-la the one Bf-109 had, some 40-50 gals?
Re the F4U, were there enough for the task in 1943, given that they were also being supplied to the USN, USMC, RN and RNZAF?
D type
This designation applied to the unarmed long-range wing for reconnaissance versions. Space for substantial amount of additional fuel was provided in the space ahead of the wing spar, which together with the reinforced skin of the wing's leading edge formed a rigid torsion box. Its otherwise empty interior was converted into an integral fuel tank capable of carrying 66 imp gallons. On hot summer days, so large amount of fuel inside the wing would produce a substantial volume of vapour, so relief valves were fitted to the tanks in the outboard rib position.