Assuming the fuel available for range is exactly that, the 15 minutes allowance is for a climb over the airfield, the fuel economy figures look too good and are inconsistent, the way the mark II is worst then best depending on speed.
Performance Tables of British Service Aircraft, Air Publication 1746, dated August 1939 but data includes 1940/41 aircraft. The ranges of fighters are shown as ranges at maximum economic cruising power on the fuel available, after deducting fuel used in 15 minutes at maximum power at sea level. This allowance is for warming up and climbing to operational height. The above makes no allowance for - (i) The effect of wind, (ii), The effect of formation flying, (iii) The use of full throttle over enemy territory. The effect of these factors must be allowed for when fights are being planned.
| Spitfire | I | IIa | Vb |
| Cruising Speed (m.p.h) | 304 | 314 | 310 |
| Cruise Speed Height | 15,000 | 15,000 | 15,000 |
| Range (15 mins allow.) (miles) | 415 | 335 | 335 |
| Fuel (for range, gallons) | 64.53 | 57.48 | 54.01 |
| Fuel (for range, pounds) | 484 | 414 | 389 |
| Fuel (for allowance, pounds) | 146 | 191 | 216 |
| Fuel (Total, pounds) | 630 | 605 | 605 |
| Fuel (Total, Gallons) | 84 | 84 | 84 |
| Miles per gallon | 6.43 | 5.83 | 6.20 |
| x | x | x | x |
| Speed (m.p.h) | 180 - 190 | 180 - 190 | 180 - 190 |
| Height (feet) | 15,000 | 15,000 | 15,000 |
| Range (15 mins allow.) (miles) | 575 | 530 | 480 |
| Fuel (for range, gallons) | 64.53 | 57.48 | 54.01 |
| Fuel (for range, pounds) | 484 | 414 | 389 |
| Fuel (for allowance, pounds) | 146 | 191 | 216 |
| Fuel (Total, pounds) | 630 | 605 | 605 |
| Fuel (Total, Gallons) | 84 | 84 | 84 |
| Miles per gallon | 8.91 | 9.22 | 8.89 |
On the above figures, give the mark I 124 gallons of 87 octane fuel and the range is around 930 miles, less deductions for carrying the extra weight, give it 100 octane and add more range (And deduct 0.3 pounds per gallon from the weight). One report I have is Spitfire I range 395 miles including combat allowance.
One RAF report gives the Mustang I with the F3R engine a range of 990 miles at 15,000 feet, with 153.2 imperial gallons of fuel, which the above figures suggests the Spitfire I could have managed with around 131 Gallons. Now the Spitfire I tare weight was around 1,640 pounds less than the P-51A empty weight but somehow it does not seem correct the energy required to move that extra weight 3 miles up comes to over 20 gallons of fuel.
| Economic cruise | VIII | IX | difference |
| Range (miles) | 660 | 434 | 226 |
| Fuel (gallons) | 124 | 85 | 39 |
| Miles per gallon | n/a | n/a | 5.79 |
Spitfire VIII cruise 20,000 feet, 320 mph, 66 gallons per hour, 4.85 mpg.
The Spitfire VIII increased internal fuel by 45.8% compared to the mark I, the P-51B increased internal fuel by 46.2% compared to the P-51A
The Spitfire 75 gallon rear fuselage tank gave problems as it had plenty of volume for the fuel to move around as the tank emptied, worsening the handling. Something similar would happen with leading edge fuel tanks, with the effects more pronounced the further outboard they are and their capacity. Comments from P-51 pilots about when they considered the rear fuselage tank fuel load was safe for combat and effects on handling as it emptied would be useful.
The Spitfire XII had the biggest engine drawing on the original fuel capacity and so the shortest range, it was meant as a low altitude fighter, to counter the Fw190 hit and run raids. The mark VIII as built has the altitude performance and matches the mid 1943 P-47 range but requires more internal fuel to match the late 1943 and early 1944 range, with that extra fuel known to be possible based on the late 1944 to early 1945 fuel carried in the rear fuselages of mark IX and XVI. By the allied standards of mid 1943 the mark VIII could be described as a long range fighter, as of early 1944 it was a medium range one.
Find the 8th Air Force fuel consumption guides for the fighters, how much fuel for what distance and how the fuel load was distributed between the available fuel tanks.
In 1943 the allied ETO air forces and Luftwaffe trained each other as the Luftwaffe pulled its fighters back to beyond allied escort range and then largely kept that deployment when allied fighter range grew further in late 1943/early 1944. It meant escort fighters could carry fuel loads that would be dangerous in combat well into enemy airspace, unlike the 1941/42 and early 1943 fighting where interception would happen near the coast.