My source is the P-39Q Pilots Manual, google it. At 25000' the P-39Q burned 62 gallons per hour at 2600rpm (maximum cruise power aka maximum continuous power), the highest cruising power available at that altitude. Full power at 25000' would cost you about 71gph. My estimate was prepared just like the manual says to plan a mission. I stand by those figures.
May I say balderdash!
As to any extra performance due to deleting wing guns from the P-39Q and going back to the four .30 cal guns.
P-39Q at sea level with drop tank.....259mph...2600rpm.......39in map.......96 gallons an hour
P-39K at sea level with drop tank.....256mph....2600rpm......37.5in map.....96 gallons an hour
Not seeing any big reduction in drag here. certainly not 10-15mph worth.
You want the performance of the 87 gallon plane but you want the endurance of the 120 gallon tank plane. Sorry, reality doesn't work that way.
you also are planning on using a 110 gallon drop tank which seems to be only slightly more common than unicorns. No mention of them in P-39 manuals. I am sure they existed somewhere but then adding another 210lbs of fuel just makes the initial climb out worse.
There is no need to guess at the fuel needed to get to 25,000ft, it is in the tables in the manuals.
for a P-39Q with a take off weight of about 8100lbs Which is close enough to our P-39X with four wing guns, 87 gallons of internal fuel and a 76 gallon drop tank (within 50lbs?) it needs 39 gallons using a combat climb and 42 gallons using a ferry climb.
ALl of these planes took of using one of the main tanks and switched to the drop tanks (subject to restrictions of CG) as soon as possible. However most of the planes arranged for any venting, overflow form the carb to go back to the main tank used for take-off so they partially filled in flight.
True test/criteria of combat radius is not how far you can get in but how far you can get back from, extra large drop tanks are no help.
after you drop the tanks you need 20 minutes at max power for the P-39, other planes were rated at 5 minutes WEP and 15 minutes at military power at altitude. P-39 can't make military power at these altitudes so take what you can get. It will suck up 82 gallons an hour at 20,000ft at nax continuous so perhaps the 71 gallons hour is an underestimate for full power at 25,000ft?
If we use the pounds of fuel per hour for military power at 15,500ft (1125hp for 138 gallons=0.736) and use it for 772hp at 25,000ft we get a consumption of 94.7 gallons an hour. Round it down to 90 or 1.5 gallons per minute.
Combat allowance is 30 gallons, leaves 57 gallons in our 87 gallon plane assuming that the return fuel fully filled the wing tank. Now you have to get the heck out of Dodge. You can fly at 224IAS (313 true) at 20,000ft using 77 gallons an hour. You do want 16 gallons or so (the reserve?) to find your own airfield and land so you have about 40-41 gallons for the withdrawal. chart says 40 gallons is good for 150 miles but you can slow down some over the Channel.
Basically you can escort a bit past Amsterdam and Antwerp. Paris might be out of reach.
cutting things too close leads to incidents Like No 133 Squadron in their Spitfires being blown off course by high winds and 11 planes out of twelve being lost.