davparlr
Senior Master Sergeant
I tend to think that after all Roosevelt did to manipulate US emotions to provide vital assets to England before US involvement in the war, Churchill would be quite compliant to a Roosevelt request for support.
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How compliant?
Swiping their Mustangs may have been going a bit too far. And to do any real good at Midway they would have had to have been swiped in Feb-March in order for training to happen, both for pilots and mechanics, and for the deployment on the squadrons/group.
VBF-13 said:What I think we need to do here is get a grip on things. Supposing they were available. So what? Do we really think subbing them for our F4Fs would have held off that incoming wave to Midway? They hit that wave, they'd have been running like rats. Even if they'd have stuck, they'd have been shot down to the last plane, and the bulk of that wave would have got through. Simply put, they wouldn't have saved that island. Neither would they have been of any use to us against those carriers.
Hey, Greg, I must respectfully disagree. You've never driven with my 17-year-old nephew in the driver's seat.Go buy a family car today and drive it for 4 years; I bet you'd have a few failures to deal with, too. And that isn't even CLOSE to combat.
Non-combat related accidents (including training) is known as attrition and is not included in the overall combat record of an aircraft, at least in today's military bean counting world, I strongly suspect it was similar if not the same during WW2.If you add in ALL the losses, including non-action sorties losses, training, etc., you'd get 1,327 victories and 1,338 total losses for an overall kill to loss ratio of 0.992.
That word is even used when weather or maintenance prevents a mission from being flown.Attrition huh? I like that word
Don't give bean counters any ideas!At least we don't have a lot of people who want to include attrition in the victory to loss ratio.
I'll introduce some heresy into the discussion. I doubt the P-51/Mustang would have done any better than the 'obsolete' F2A-3's everyone seems so anxious to dump into the ocean to make room for a 'real non-obsolescent fighter'. First let's consider the mission. The F2A-3s, for better or worse, were committed to act as interceptors. I submit that speed is one of the least useful attributes of an interceptor. In order of importance I'd list
1. Rate of climb: I can't say it any better than Bedford Forrest: "get thar fustus with the mostest" Not fastest, just fustest.
How long does it take the Mustang I to climb to the enemy aircraft altitude before it can accelerate to its speed advantage?
I believe the F2A-3 and Mustang had very similar to nearly the same rate of climb to the altitude of the engagement. Above that altitude, advantage F2A-3. Shocking, I know but the lighter weight F2A-3 had a single stage, 2 speed supercharged Wright 1830 radial engine of 1,200 SL hp. The Mustang/P-51 was laboring with an Allison 1710-39 engine of 1,150 SL hp with a single stage, ONE-speed supercharger.
2. Ceiling: This is not a critical factor at Midway since the combat was fought at intermediate altitude (I think about 20,000 '), but in general you want to get an interceptor high so it can quickly convert that potential energy into kinetic when it sees the enemy, but the tendency would be to maintain the climb as long as possible until you have to engage.
1st AVG did not do this. They were warned by Chennault to avoid this type of combat. Slash and run was used and proved effective. P-38s also perfected this combat.3. Acceleration: Once you've engaged in a first pass, the interceptor is going to find itself in a fur ball when the enemy escorts jump you.
If you've built up speed so much the better, but I suspect that may be problematic in an interception. What you need before speed is to get to max speed quickly. The Mustang (2 cannon version) is about 1,000 lbs heavier than an F2A-3 (the 4 cannon mustang is nearer 1,500 lbs) with a similar powered engine. Simple physics says the same force applied to a smaller mass will accelerate it faster. I admit that the F2A's higher drag limits this advantage and its ultimate speed. But in the pinch, I suspect the P-51 is going to be bit slower off the mark. Not a good thing vs the IJN Vet piloted A6M.
4. Maneuverability: I expect the F2A may have held an edge over the Mustang but they were both at a disadvantage compared to the A6M.