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Not strictly true; I forgot to mention that the fuselage tank could only be used in conjunction with the 170 gallon ferry tank (it's in the A.P.)In case the 30 gal drop tank is attached under fuselage of the Spit V, and there is no extra fuselage fuel, max fuel is 30+84=114 imp gals. If the 29 gal tank is installed, max fuel can be 113 imp gals plus whatever is attached under fuselage (from 30 to 170 imp gals) - from 143 to 283 imp gals.
Any fuel tank in any aircraft is full of volatile fumes when half or full empty, that goes also for the fuselage tank of the Mustang III/IV, and LE tanks of the later Spitfires (unless the fumes are purged by CO2 that some aircraft have had).
In case the 30 gal drop tank is attached under fuselage of the Spit V, and there is no extra fuselage fuel, max fuel is 30+84=114 imp gals. If the 29 gal tank is installed, max fuel can be 113 imp gals plus whatever is attached under fuselage (from 30 to 170 imp gals) - from 143 to 283 imp gals.
Not strictly true; I forgot to mention that the fuselage tank could only be used in conjunction with the 170 gallon ferry tank (it's in the A.P.)
And here we get into part of this argument. Timing.
The MK V Spitfire had the good propeller and it had The Merlin 45 engine. The Merlin 45 could hold 9lbs boost to 20,000ft with ram compared to the Merlin III holding 6lb boost to 18,000ft with ram, The Merlin 45 could hold 6lbs of boost to 23,000ft. It also had about 300 more HP for take-off (34%) All for very little increase in weight in the power plant.
You now have the power to lug around a bit more weight without taking a big hit to performance. I would note that tests of a "normal" Vb and a MK V with 4 20mm guns show the 4 cannon fighter losing about 340fps (about 10%) in climb and about 1000-1100ft in ceiling. At 28,000ft the loss in climb was about 13-14%. Part may be drag but weight has more influence on climb.
the 4 cannon MK V climbs about like MK II Spitfire. If that is good enough so be it.
30 Imp gallons was good for about 1 hour at a very economical cruise speed. A speed that would be near suicidal to use over enemy territory or in enemy coastal waters. Where over the Channel you cut from the higher cruise to speed to the economical cruise speed may be a matter of argument but 20imp gallons may not get you a radius that includes the Ruhr or much of it.
With the Americans in charge the campaign against oil may the war may have been shortened considerably. Now this view is certainly counterfactual and laced with hindsight, but hopefully some will find it worthy of the forum.
Regards
Well, let's see...
The RAF:
Lancaster I - (2) .303 nose turret, (2) .303 upper turret, (4) .303 rear turret
Halifax Mk.III - (1) .303 nose, (4) .303 dorsal turret, (4) tail turret
Stirling I - (2) nose turret, (2) dorsal turret, (4) tail turret
Lincoln I - (2) .50 nose turret, (2) .50 OR (2) 20mm dorsal turret, (2) .50 tail turret
The U.S.:
B-18A - (1) .30 nose, (1) .30 dorsal, (1) .30 ventral
B-17F(early) - (1) .50 nose, (2) .50 "cheek", (2) .50 dorsal turret, (1) .50 radio skylight, (2) .50 waist, (2) .50 ball, (2) .50 tail
B-24D - (3) .50 nose, (2) .50 dorsal turret, (1) .50 tunnel, (2) .50 waist, (2) .50 tail
B-25C/D - (1) .30 nose, (2) .50 dorsal turret, (2) .50 ventral turret, (2) waist (optional), (1) .50 tail
B-26B - (1) .50 nose, (2) .50 dorsal turret, (2) .50 waist, (2) .50 tail
In comparing 4 of the RAF's bombers against 5 of the U.S., I am having difficulty in seeing how the RAF was "on a par" with the U.S. heavy bombers. So I looked at the U.S. medium bombers and lo and behold...the medium bombers were comparable. (Except for the B-18, I just tossed that in for the heck of it!)
Bottom line, the U.S. heavy bombers were heavier armed, both in caliber and quantity, than their RAF counterparts.
With the exception of the Lincoln, the RAF bombers were woefully under-gunned, no matter how you look at it.
I entirely accept that the 50cal had a longer range and more hitting power than the .303, as I made clear in my previous post.
On the contrary, there was room and the Bombadier and the Navigator manned the foreward (nose - cheek) MG positions. The Engineer manned the dorsal turret and the Radio Operator manned the spine position.For example, only one gun of the 3 in the noses of the B-17F and B-24D could be fired at one time because there was only one guy in there to do the shooting.
There's a good bit of truth to the long-range vs short range fighter capability. However, when the interceptor is tasked with avoiding the escort and reaching the bombers, the balance changes. With dissimilar resources, both people and material, the balance further changes. This wasn't apparent in early 1941. The ugly duckling P-51A was not left to fade away only by its improbable conversion to the A-36.
If foresight is lacking, it helps to be agile –and lucky- on the rebound.
The Luftwaffe went to great lengths to defeat the B-17's (and to a certain degree: the B-24) defensive armament. You may have seen photos of the wire-frame "defensive cones" on scale models of B-17s and B-24s in use by the Luftwaffe flight school.
Apologies for being late into the thread but in 1944 the RAF did at least one daylight raid from the UK to the Rhur using Halifax bombers escorted by Tempests. The Tempest didn't have the range of the P51 but it had sufficient range to escort raids capable of inflicting significant damage.The great thread on "Innovative to Obsolete" made me think of this question and I didn't want to muddle up that topic.
Did the RAF have a design or an airplane that could perform the duties the Mustang ended up performing? I know the RAF mostly carried out the night-time bombing of the Third Reich and I guess (ignorant on the information here) they didn't utilize escorts on these missions.
Were they working on, or did they have, a daytime long ranger fighter?
Not once you put the radio IFF gear back in, plus armour, which the P.R. aircraft normally didn't carry.The 170 gal tank was also drop-able. For the Spitfire there was also a possibility of having an under-seat fuel tank installed (closer to the CoG than the rear fuel tank), used on some early PR machines? .
If you mean the tanks in the leading edges, they couldn't be fitted to the V, and were only on the VII, VIII, XIV XVIII, not the IX (or XVI for that matter.)There was also possibility of 10 extra gals in the front tank(s), that was used to that cause in Mk VIII and modified Mk IXs, among other
The props were fitted by de Havilland teams, travelling across the country, just before the start of the Battle.The de Havilland 2-pitch prop was installed in a number of Spitfires prior ww2 broke out, there is a picture of such Spitfire Is at the Morgan Shacklady book, pg. 54, dated 8th June 1939. Constant speed props were installed in 1940?
If you mean the tanks in the leading edges, they couldn't be fitted to the V, and were only on the VII, VIII, XIV XVIII, not the IX (or XVI for that matter.)