Shortround6
Major General
A problem when trying to compare P-40s is that they change a lot in the early ones.
IF you could get a P-40 to go 730 miles on internal fuel it was an early one without self-sealing tanks or tanks with a crude sealing applied outside, capacity 160 US gallons. Getting one to go 1270 miles if throttled back requires a real leap of faith. 3 times the range of a Spitfire or 109 on 60% more fuel? Those P-40Bs must have been one slick ship
P-40D/E was rated for 700 miles on 120 US gallons (100imp) remaining with 28 US (23imp) used for warm up and take-off at 173-188mph indicated depending on altitude, sea level to 15,000ft. I am not sure you want to throttle back any more than that. Max endurance is often NOT max range.
At a more useful 229mph indicated at 15,000ft range for the 120 US gallons was 425 miles. Fuel burn was in the 70-80 gallon an hour range depending on altitude.
Some the early performance numbers are a little suspect. this test report has some very good numbers. Trouble is it gives the gross weight of the plane at 6835lbs which is either a misprint or there is a whole lot of "stuff" not in the airplane.
A P-40B with full internal tanks, full ammo and NO external tank could go 7624lbs. A P-40C with external tank could go just over 8000lbs.
http://www.wwiiaircraftperformance.org/P-40/P-40B_41-5205_PHQ-M-19-1227-A.pdf
Some of the P-40s 'success' in North Africa and with the AVG came from over-boosting the engines in service. This only worked at low altitudes and could not be used at the altitudes the bombers were flying (the supercharger simply would NOT supply the higher pressure at those altitudes.)
P-40s climb, unless being over boosted (or running light, ie little ammo or fuel) at low altitudes is best described as mediocre and falling to dismal at higher (in this case 15,000ft and above) altitudes.
A lot is made of speed and while I don't subscribe to the view that is as unimportant as some do it, others focus on it to exclusion of rate of climb. Rate of climb, while not linear, is an indication of acceleration and/or the excess power available to to sustain speed through maneuvers. The Bf 109 gun boats lost very little speed it is true, but they lost rate of climb (and losses in rate of climb tend to carry through to the higher altitudes. a 10% loss in rate of climb at sea level is often a 15-20% loss in rate of climb in the 20-30,000ft range) and turning ability.
An equipped, loaded P-40B at 15-20,000ft is no match for a 109. And you can't escort bombers flying at 12-15,000ft by flying at 6-9,000ft.
and as always, drop tanks are for getting you in, internal fuel is for getting you out. adding drop tanks but not adding internal fuel doesn't do a lot for radius past a certain point.
IF you could get a P-40 to go 730 miles on internal fuel it was an early one without self-sealing tanks or tanks with a crude sealing applied outside, capacity 160 US gallons. Getting one to go 1270 miles if throttled back requires a real leap of faith. 3 times the range of a Spitfire or 109 on 60% more fuel? Those P-40Bs must have been one slick ship
P-40D/E was rated for 700 miles on 120 US gallons (100imp) remaining with 28 US (23imp) used for warm up and take-off at 173-188mph indicated depending on altitude, sea level to 15,000ft. I am not sure you want to throttle back any more than that. Max endurance is often NOT max range.
At a more useful 229mph indicated at 15,000ft range for the 120 US gallons was 425 miles. Fuel burn was in the 70-80 gallon an hour range depending on altitude.
Some the early performance numbers are a little suspect. this test report has some very good numbers. Trouble is it gives the gross weight of the plane at 6835lbs which is either a misprint or there is a whole lot of "stuff" not in the airplane.
A P-40B with full internal tanks, full ammo and NO external tank could go 7624lbs. A P-40C with external tank could go just over 8000lbs.
http://www.wwiiaircraftperformance.org/P-40/P-40B_41-5205_PHQ-M-19-1227-A.pdf
Some of the P-40s 'success' in North Africa and with the AVG came from over-boosting the engines in service. This only worked at low altitudes and could not be used at the altitudes the bombers were flying (the supercharger simply would NOT supply the higher pressure at those altitudes.)
P-40s climb, unless being over boosted (or running light, ie little ammo or fuel) at low altitudes is best described as mediocre and falling to dismal at higher (in this case 15,000ft and above) altitudes.
A lot is made of speed and while I don't subscribe to the view that is as unimportant as some do it, others focus on it to exclusion of rate of climb. Rate of climb, while not linear, is an indication of acceleration and/or the excess power available to to sustain speed through maneuvers. The Bf 109 gun boats lost very little speed it is true, but they lost rate of climb (and losses in rate of climb tend to carry through to the higher altitudes. a 10% loss in rate of climb at sea level is often a 15-20% loss in rate of climb in the 20-30,000ft range) and turning ability.
An equipped, loaded P-40B at 15-20,000ft is no match for a 109. And you can't escort bombers flying at 12-15,000ft by flying at 6-9,000ft.
and as always, drop tanks are for getting you in, internal fuel is for getting you out. adding drop tanks but not adding internal fuel doesn't do a lot for radius past a certain point.