Apologies for tagging a belated tangent onto an interesting discussion, but one thing that probably needs to be ascertained is what the performance of the Skua actually
was.
The quoted 225 mph looks suspiciously rounded, and I'm not sure how to establish whether this is a design specification, a figure obtained with the Mercury XII engine on the prototype (830hp on takeoff, 890hp at 6,000ft, 51.5" diameter, and a weight I can't find stated, but presumably approximately 1000lbs) or a service speed with the theoretically draggier and less powerful Perseus XII (830hp on takeoff, 750hp at 6,500ft, 55.3" diameter, 1025lbs).
This 225 mph figure is often quoted as the speed at 6,500ft, i.e. the optimised altitude of the Perseus XII, but this may be an extrapolation based on the assumption that that's the natural height to peg the figure to; in contrast,
Peter Caygill's Flying To The Limit, presumably using RAE dociments, says 225 mph is actually a
sea-level figure, which looks very like a design specification, but on the other hand, should perhaps improve with altitude. The Roc, with the Perseus XII and a draggy turret, is quoted in the same source at 223 mph at 10,000 feet - would the Skua be expected to do a bit better?
Moreover, as these number suggest, the supercharger on both motors was optimised for a relatively low altitude, so I'd imagine a motor optimised for high-level performance would get a slightly better top-line speed, simply because good power at high altitude translates to higher speed in the thinner, less draggy air.
The question is, what motor? There's definitely room for improvement, if both the engines the Skua was flown with were too light for the airframe, and had to be jettied out two and a half feet ahead of the firewall - does that indicate something about the design process? How much more can be got out of a single-row radial? Would one of the big twin-row radials in the 2,000lb weight class, powerful but half-a-ton heavier and correspondingly thirsty, be practical, or would a Merlin be a better alternative than any of them? The Bristol Taurus, a small twin-row, weighs not much over 1250lbs and gives around 1100hp, but it's optimised for 5,000ft and at closer to 45" diameter, would it be to small? Apparently Alvis had a licensed version of the Gnôme-Rhone Mistral Major with a 52" diameter and a weight of under 1200lbs which gave over 1,000hp on the bench and had a high-altitude supercharger, all tooled-up with nowhere to go because the Air Ministry couldn't think of a good use for it...
And quite apart from engines, there's something to be said for a better propeller - the Skua used a two-speed prop, where the blades could pivot between two settings, one for take-off power and the other either for most-economical cruise or fastest possible dash, I'm not sure which; I've seen it said that it could be manually set at angles between the two extremes, but I'm not sure if that's true, and the general view seems to be that automatic "constant-speed" units handled such variation better than the average pilot, giving both a quicker climb and faster acceleration from manoeuvres in a fight.
And what else could be improved? Is there something to be gained in swapping the back-seater, who only seems to be there for morse-code messages and conversation, for seatback armour and a sleeker cockpit canopy? Can we get something with more fighter-like performance that still dive-bombs? And if so, which fighter does it equate to? The Gladiator? Fulmar? Sea Hurricane?
Everyone should feel free to brutally demolish any nonsense in what I've written - I'm really just an observer from the ground, and may only be showing my ignorance...
But, set up like a row of coconuts, a few more random observations on topics that have been raised in this discussion:
* A 500lb SAP/GP is probably less than ideal in a naval role; but the limited weight can be compensated for by doing what the IJN's Vals did repeatedly, mob targets with a reasonably large number of planes - as to the effectiveness of the tactic against armoured capital ships, the obvious example is USS
Nevada, caught by a half-dozen Val hits that would have foundered her if she'd been on the open sea and unable to beach herself; HMS
Warspite was sent to the rear for almost year by a couple of 500lb hits from Bf 109s, albeit
Graf Zeppelin's specially-trained CAG, the Luftwaffe having decided that they didn't need to bother with the boat... beyond that, there simply aren't many examples, as the IJN switched to useless skip-bombing A6Ms and no-one sent Skuas against
Tirpitz... but on the other hand, while the effects of
a near miss by a large blast-bomb, raised in the previous Skua thread, certainly
look impressive, the punchline there is that
no-one actually noticed...
* BuShips damage analysis may not be very reliable at any level more detailed than "big jagged hole in the hangar deck"; I've seen all kinds of things misidentified as hits on opposing capital ships by US Navy battleship main-guns, including a pair of 1,000lb bombs from SBDs (
Jean Bart at Casablanca, 1942)...
* The one RAF aircraft that could and did dive-bomb was, of all things, the Westland Whirlwind, which dropped pairs of 250lb in an 80° dive (I think using the trim tabs to recover); why a twin-engined high-altitude interceptor was given this capability I do not know, except that it seems a very Petter thing to do. The problem with overspeeding mentioned in some sources was caused by an unsatisfactory two-pitch prop, which de Havilland solved on a wet wednesday in the Battle of Britain by clocking the blade angle round by about three degrees, but I don't think they ever got a constant-speed unit, which explains why they never met their design performance in the high-altitude interceptor role...
* Speaking of the advantages of large, thin-skinned blast-bombs, and random things that de Havilland did on their own initiative in 1940...
Seems badly assembled bombs would not drop straight or would lose their tails, some Germans actually asked the US investigators post war what experiments were the allies doing with tail less bombs, which gives an idea of how often it happened.
Is it possible that Luftwaffe officers were asking about the fact that Berlin had been reduced to rubble by two-ton drums of HE toted by unusually-shaped flying pianos?
But I get the sense that Pathfinder Force didn't even tell Bomber Command what they were doing, so it's understandable that the USAAF might be confused...
The version I've read is that their lack of aerodynamics actually made them more accurate, as they didn't tend to "fly" like the finned equivalent. Those with more knowledge than me might want to comment on the plausibility of this claim?