According to Roger Freeman, B-17B
3,600 miles at 176 mph at 10,000 feet with 2,496 gallons of fuel, no bombs, weight 45,650 pounds
2,400 miles at 230 mph at 25,000 feet with 1,700 gallons of fuel, 4,000 pounds of bombs, weight 44,500 pounds
1,300 miles at 230 mph at 25,000 feet with 850 gallons of fuel, 2,400 pounds of bombs, weight 37,000 pounds
Non Tokyo Tank B-17F 1,300 miles at 200 mph at 10,000 feet with 1,730 gallons of fuel, 6,000 pounds of bombs, weight 56,500 pounds
Tokyo Tank B-17F 2,200 miles at 200 mph at 10,000 feet with 2,810 gallons of fuel, 6,000 pounds of bombs, weight 65,500 pounds
Assuming the 1/3 rule, Non Tokyo B-17 radius above would be around 450 miles, with 8th Air Force tactics it was 320 miles, at 225/240 mph at 25,000 feet, 6,000 pounds of bombs. 1,760 gallons of fuel, 380 gallons used in climb, all up 1,075 gallons used to target, 115 gallons remaining on return.
Aerodynamics matters, Hurricane I economic cruise 7.73 mpg, Spitfire I 8.91 mpg, 15% more efficient
Gauntlet 15 minutes allowance = 12.4 gallons take off and climb to 15,000 feet
Gladiator II 15 minutes allowance = 18 gallons take off and climb to 15,000 feet
Hurricane I 15 minutes allowance = 19.4 gallons take off and climb to 15,000 feet
Spitfire I 15 minutes allowance = 20 gallons take off and climb to 15,000 feet
Spitfire VIII actual 23 gallons take off and climb to 20,000 feet, 54 gallons for combat and reserves.
The allowances seem to over estimate the Spitfire I requirements at least.
100 octane weight 7.2 pounds per gallon, allowance is fuel used in 15 minutes maximum power at sea level for warming up and climbing to operational height. Cruise height 15,000 feet, take off weight excludes external fuel, radius is for the aircraft released at 15,000 feet with running engine and full fuel tanks. Assumptions: external tanks are weightless and cost 10% of their fuel due to drag but do not drop speed and carry the fuel needed for the allowance and fly to radius distance. The final Spitfire column uses the mark VIII forward fuselage fuel capacity, 96 gallons to show what a seemingly small change in internal fuel does, radius at 305mph would be around 360 miles. The Spitfire Vb clean take off weight was 6,460 pounds, the Hurricane IIc 7,544 but with more power available. The US types have a protection problem.
| Aircraft | Mohawk | Mohawk | Tomahawk | Tomahawk | Gauntlet | Gladiator | Hurricane I | Hurricane I | Spitfire I | Spitfire I | Spitfire I |
| Clean Take off Weight lb | 7,000 | 7,000 | 7,602 | 7,602 | 4,028 | 4,912 | 6,661 | 6,661 | 6,255 | 6,255 | 6352.5 |
| Cruise Speed (m.p.h) | 185 | 248 | 185 | 278 | 118 | 142 | 170 - 180 | 281 | 180 - 190 | 305 | 180 - 190 |
| Fuel weight pounds/gallon | 7.2 | 7.2 | 7.2 | 7.2 | 7.7 | 7.5 | 7.5 | 7.5 | 7.5 | 7.5 | 7.5 |
| Internal fuel gallons | 132 | 132 | 132 | 132 | 79 | 83 | 97 | 97 | 84 | 84 | 96 |
| clean range with 15 mins allowance | 800 | 592 | 800 | 615 | 511 | 488 | 580 | 447 | 575 | 415 | 681 |
| allowance gallons | 29 | 29 | 25 | 25 | 12.60 | 17.99 | 19.40 | 19.40 | 19.47 | 19.47 | 19.53 |
| mpg | 7.77 | 5.75 | 7.48 | 5.75 | 9.43 | 8.04 | 7.73 | 5.76 | 8.91 | 6.43 | 8.91 |
| fuel for combat+reserve gals | 40 | 40 | 40 | 40 | 27 | 34 | 40 | 40 | 40 | 40 | 40 |
| radius miles | 714.56 | 529.00 | 687.85 | 528.79 | 490.27 | 394.17 | 440.72 | 328.32 | 392.05 | 282.92 | 499.19 |
| external fuel gals | 133.10 | 133.10 | 128.70 | 128.70 | 71.06 | 73.68 | 84.04 | 84.04 | 69.81 | 69.81 | 83.09 |
| external fuel wt lb | 958.32 | 958.32 | 926.64 | 926.64 | 547.19 | 552.63 | 630.30 | 630.30 | 523.60 | 523.60 | 623.16 |
| total fuel gals | 265.10 | 265.10 | 260.70 | 260.70 | 150.06 | 156.68 | 181.04 | 181.04 | 153.81 | 153.81 | 179.09 |
| Take off weight | 7958.32 | 7958.32 | 8528.64 | 8528.64 | 4575.19 | 5464.63 | 7291.30 | 7291.30 | 6778.60 | 6778.60 | 6975.66 |
| %extra weight of external fuel | 13.69 | 13.69 | 12.19 | 12.19 | 13.58 | 11.25 | 9.46 | 9.46 | 8.37 | 8.37 | 9.81 |
Using these simplistic calculations the amount of fuel carried does not change with cruise speed, the radius drops. The extra weight carried could be compensated to an extent by constant speed propellers and proper runways (see the B-24 take off charts), going to 100 octane would give more energy in the fuel for a few pounds less weight, probably around what the external tank and fittings would weigh.
The USAAF calculated the combat radius figures on internal fuel as follows, P-38J 300 gallons 125 miles, 410 gallons 275 miles, P-47D 305 gallons 150 miles, 370 gallons 250 miles, P-51B 180 gallons 175 miles, 265 gallons 400 miles. Conditions, Escort fighter accompanying B-17 at 185 mph IAS, Full power (max continuous) climbing to 25,000 feet, Cruise at 210 mph IAS, 300 mph TAS, Tanks dropped when empty or at radius, 15 minutes combat at military power, 5 minutes combat at war emergency power, Return to base at required cruising speed, accompanying bombers, 30 minutes fuel reserve.
The P-38 with 300 gallons internal could only use 175 gallons of external fuel, unless it wanted to loiter within 350 miles from base or run out of fuel going home.
The A6M in 1940? The P-51 in 1941 once it had drop tanks? Both medium altitude types. The P-51B with 180 gallons internal could only use 135 gallons external, but had a radius of 500 miles. Plenty of He111 performance figures to choose from, early H 1,200 miles with full bomb load.
The unspoken condition, escort for USAAF B-17 and B-24 types at high altitude.
Decent fighter is at least partially defined by the opposition quality, the P-36 and P-40 as escorts would have had problems with Bf109E in 1939/40 then again like the Spitfire V in 1943, if there were enough bombers the interceptors would often try and avoid engaging escorts, making the escorts competitive. Part of the 8th Air Force success was numbers, not just quality.
US Archives Record Group 342 Entry P26 Box 2237. Decimal hours 0.333 = 20 minutes. P-38F 290 gallons internal, 300 gallons external fuel,
1. Warm up taxi, take off to 100 feet 12 gallons main tanks,
2. 100 to 15,000 feet 34 gallons, 0.16 hours, belly tank
3. cruise 2,280 RPM full throttle, 250 mph, 110 gallons per hour, 2.0 hours, 220 gallons, 500 air miles flown, belly tank,
4. Drop belly tank, with 46 gallons still in it (or use the fuel but stay within 500 miles of base)
5. combat full military power for 10 minutes, 42 gallons,
6. return cruise as per outgoing but at 280 mph, 196 gallons, 1.8 hours, 500 miles,
7. Reserve 40 gallons 0.333 hours.
AFHRA Reel A2069 page 1574, P-51B with 180 internal, 150 external gallons, combat radius as fighter 350-500 miles, as escort 250-350 miles, with 265 internal and 216 external radius as fighter 700-850 miles, as escort 500-600 miles. P-38J 290 internal 300 external radius as fighter 300-450 miles, as escort 200-330 miles, P-38J with 410 internal and 300 external radius as fighter 550-700 miles, as escort 375 to 475 miles.
The P-51B with 265 gallons internal and 150 external could go out to 750 miles radius, compared to the B-17G of 2,000 miles range at 182 mph at 10,000 feet with 6,000 pounds of bombs. It also helped fighters were no longer sticking with a given bomber formation thereby forgoing range by having to weave. The 1943 problem solved, now what about escorts for the new 1944 model, the B-29?
Over and above the engineering that favoured multi engine aircraft having longer ranges comes bombers had 2 range deductions, the fuel needed to take off and climb to height and the reserves, fighters had a third, combat allowance which was expensive, even at fast cruise speeds it was worth a couple of hundred miles of range.
The bigger the aircraft the general rule the longer it takes to develop and then build in numbers. As fighters are smaller it gives them a chance to pass. In order to have the bomber force it did the USAAF had to use 1,200 HP class engines in the B-17 and B-24, while the fighters could fit more powerful engines and then carry more fuel. Add the P-51 was a real advance in aerodynamics and construction, including providing more internal room for fuel tanks. The inevitable downside is changes tend to delay mass production, made worse because the B-17 and B-24 programs had head starts.
The USAAF had P-38 in early 1943 that could escort 8th Air Force B-17 all the way to target, at least until Tokyo tank versions became numerous and in mid 1943 the P-51B which could go almost everywhere the 8th Air Force then wanted to go, it took until early 1944 before the 8th Air Force had the two fighters in numbers. Meantime in the Mediterranean from late 1942 the standard US heavy bomber mission stayed within escort range, with some obvious exceptions, like Ploesti, or could get away without (many) escorts due to a lack of axis fighters in the target area or en route.