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You're talking about the Spiteful?
The data I have suggest that it didn't have a long-range capability. To me, it's simply the successor of the Spitfire. Development started rather early but was always put on low priority. The British - more than others - upgraded existing designs rather than start with a new one. Worked well in WW2...
Kris
The XP-47J with an R-2800C-57 (2,800hp) hit 507mph in combat trim. The secret - It's combat loaded weight was 2,000lbs less than a P-47D and it had a close fitting cowl that presented a more efficient shape.
The Heinkel He P 1076 had a theoretical speed of 546 mph and forward swept wongs, so in theory it would have had a relatively small turning circle.
Heinkel He P.1076
Mark XIV - the type 371 was fitted with a Griffon 69 engine rated at 2,375 hp driving a 5 blade propeller. The top speed was 475 mph. 19 were built. Of these aircraft 1 was converted to a Mark XV and 2 were converted to Mark XVI.
Mark XV - Fitted with a Griffon 89 or 90 engine rated at 2,350 hp and driving two contra rotating three blade propellers. The one converted aircraft, RB520, was subsequently used in the development of the Seafang. Top speed was 483 mph.
Mark XVI - The two conversions from the Mark XIV, RB516 and RB518 were fitted with the Griffon 101 engine producing 2,420 hp and a top speed of 494 mph.
Talking of spit development. Wasn't their an atempt to significantly improve the the Spits range for bomber secort which ended in failure?
Davparl, wouldn't you consider the Spiteful aerodynamically more refined and lighter in weight than the P-51D?
And the tandem engine configuration of the Do 335 was aerodynamically inefficient, as acknowledged by the Dornier guys themselves.
Kris
Davparlr,
I didn't notice the P-51 was modified that way.
As to the Do 335, the problem was that the front prop couldn't achieve its maximum efficiency because the air flow interrupted that of the other engine ... or something like that
But it's obvious when you look at the next Do 335 designs: they abandoned the tandem engine layout in the P 247 and P 252.
Kris
Here's the consumption figures achieved under Australian testing of the Spitfire VIII with Merlin 66:
This aircraft had 123 gallons internally, and a 90 gallon drop tank. The drop tank remained attached at all times, hence the "ferry" designation.
If you`d add up the claimed mileage in Hop`s paper with the fuel tankage, ie. 10 mpg and 120 gallons available, this would give you something like 1200 miles (!!!) of range for the Spitfire. If this would be true, there would be never any need for the Mustang as Spitfires would easily reach out to Berlin and back.
From the Spitfire IX/XVI manual:The rear tanks, fitted irregularly to some planes at the very end of the war
were similiar to droptanks, as they could be used for ferry (one-way) missions only, like Malta.
The reason was that with the rear aux. tanks the Center of Gravity shifted so far back that the plane was outright difficult and dangerous to fly, not to speak air combat. Therefore the rear tank, like a droptank, had to be emptied first,
and then return on the normal internal tankage, again 85 gallons on the vast majority of Spits.