SpicyJuan11
Senior Airman
Which R-4360 based design had the best potential as a true fighter to take on the next wave of piston-engined Axis designs in mid-late 1945? By that I mean Fw 190A-10 (BMW 801F), Fw 190D-13/D-15, Ta 152C/Ta 152H, Bv 155C. Do 335, A7M, J6K, Ki-100, N1K5.
The point here isn't asking "what if XF8B vs Ki-100", I am asking which American design, the F2G, XF8B, or XP-72 had the best potential to be fully developed into a fighter.
The F2G didn't have the water injection of the XF8B, but if it had, would it have been faster? Was the XF8B a "jack of all trades, master of none" as a "5 in 1" fighter with its own internal bomb-bay?
Was there any advantage in having a massive R-4360 powered fighter when compared to the other alternatives coming online in 1945 (P-51H, XP-47H, F8F, etc).
Obviously jets were coming into service anyways, but for the sake of discussion (that is, the discussion of the future course of piston-engined fighters), let's assume they aren't a factor in any way.
I don't have any references at hand, so here is a quick summary of the different aircraft's performance based on wikipedia (which I'm sure will be corrected)
Empty Weight
XF8B - 13,500 lbs
XP-72 - 11,500 '
F2G - 10,250 '
Max takeoff weight
XF8B - 21,700 lbs
XP-72 - 17,500 '
F2G - 15,400 '
Powerplant
XF8B - 3,600 hp XR-4360-10
XP-72 - 3,500 hp R-4360-13
F2G - 3,000 HP R-4360-4
Max Speed
XF8B - 450 mph
XP-72 - 490 '
F2G - 430 '
Rate of Climb
XF8B - 2,000 ft/min
XP-72 - 5,280 ft/min '
F2G - 4,400 ft/min
Service Ceiling
XF8B - 37,500 ft
XP-72 - 42,000 '
F2G - 38,800 '
Wing Loading
XF8B - 41.9 lb/sq
XP-72 - 48.1 '
F2G - 42.5 '
A very interesting note by wiki:
How would the F2G have performed with such an engine? Would it have blown the F4U-5 out of the water?
The point here isn't asking "what if XF8B vs Ki-100", I am asking which American design, the F2G, XF8B, or XP-72 had the best potential to be fully developed into a fighter.
The F2G didn't have the water injection of the XF8B, but if it had, would it have been faster? Was the XF8B a "jack of all trades, master of none" as a "5 in 1" fighter with its own internal bomb-bay?
Was there any advantage in having a massive R-4360 powered fighter when compared to the other alternatives coming online in 1945 (P-51H, XP-47H, F8F, etc).
Obviously jets were coming into service anyways, but for the sake of discussion (that is, the discussion of the future course of piston-engined fighters), let's assume they aren't a factor in any way.
I don't have any references at hand, so here is a quick summary of the different aircraft's performance based on wikipedia (which I'm sure will be corrected)
Empty Weight
XF8B - 13,500 lbs
XP-72 - 11,500 '
F2G - 10,250 '
Max takeoff weight
XF8B - 21,700 lbs
XP-72 - 17,500 '
F2G - 15,400 '
Powerplant
XF8B - 3,600 hp XR-4360-10
XP-72 - 3,500 hp R-4360-13
F2G - 3,000 HP R-4360-4
Max Speed
XF8B - 450 mph
XP-72 - 490 '
F2G - 430 '
Rate of Climb
XF8B - 2,000 ft/min
XP-72 - 5,280 ft/min '
F2G - 4,400 ft/min
Service Ceiling
XF8B - 37,500 ft
XP-72 - 42,000 '
F2G - 38,800 '
Wing Loading
XF8B - 41.9 lb/sq
XP-72 - 48.1 '
F2G - 42.5 '
A very interesting note by wiki:
Test pilot Tom Bellinger stated flatly that his no flights ever exceeded 500 mph with the dash 13 engine. With the planned but never installed dash 19 engine rated at 3,650 HP at 25,000 ft (3,000 HP at military power) a top speed of 504 mph at approximately 25,000 feet was expected. Planned further development of the dash 19 engine was expected to yield approximately 4,000 hp and a speed of 540 mph at 25,000 ft.
How would the F2G have performed with such an engine? Would it have blown the F4U-5 out of the water?