Spitfire Mk.XIV vs P-51D Mustang

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This is interesting about the Specifications possibly being adjusted to fit the prototype. Seems backwards
Actually happens often in oil field engineering. All specifications are written in cooperation with manufacturers, otherwise you specify what cannot be done, then you issue a new spec for what can be done, if you catch my drift.
 
Wasn't the Supermarine 300 submitted to the same specification? I may be wrong. My main point being that the Spitfire wasn't specifically built to be an interceptor.
The Spitfire and Hurricane were designed for speed and climb which in my view is the basis of an interceptor. Clearly the Spitfire was far ahead but remember that when the Hurricane first entered service, there was nothing anywhere to touch it.
 
Also from wiki...
" On 3 January 1935, they formalised the contract with a new specification, F10/35, written around the aircraft. "
 
The Spitfire and Hurricane were designed for speed and climb which in my view is the basis of an interceptor
It would be interesting to see if time to altitude requirements were incorporated into the specification.
Anyway, would you still consider the Hurricane to be an interceptor? Certainly not by 1942, but again, I may be wrong.
As far as I remember, both aircraft (Hurricane and Spitfire) were designed to be fast monoplanes, with retractable gear, and able to destroy an enemy aircraft in one pass.
EDIT:
With eight .303 Brownings being almost unheard of firepower in 1935
 
Maybe not initially, but that's what it was developed into, the Mustang was never developed into that role...


Ah, did it need to be?
P-51Bs without drop tanks could go from sea level to 20,000ft in under 7 minutes (one test 5.9 minutes) which if not quite as fast as a contemporary Spitfire is several minutes faster than the Spitfires of 1940.
How fast did a 1943 "interceptor" need to get to 20,000ft in given the improvement in radar warning in 1943 vs 1940?

If, in 1943, the difference between on fighter making it to 20,000ft 5 minutes and another making it 6 minutes actually affected the success of the intercept then something was wrong with radar warning or the vectoring from fighter control.
 

The specs for the Hurricane and Spit were designed around the aircraft. Re the question on the Hurricane remember we were discussing the design and I have no doubt that both were designed as interceptors.
A personal view is that the Hurricanes time as an effective interceptor was mid / late 1940, by 1942 it was well past its best when compared to other nations, but when it entered service, it didn't have to apologise to anyone. It just shows how technology was speeding up.

My brother often points out that Gloster went from the Gladiator to the Meteor. They did other designs in betwee,n but none that I can think of entered serious production.
 
By the fall of 1940 the Hurricane was in trouble and they knew it, which is why the Hurricane got the Merlin XX engine. It was an attempt to keep the Hurricane competitive while newer fighters (Typhoon?) were built. Since the Spitfire was faster and climbed better it could make do with a 2nd best engine a bit longer.
The plan went to pot when the Germans didn't just stick a more powerful engine in the 109E but developed the F with much lower drag and then the Germans frosted the cake with the FW 190. The Hurricane, useful as it was in other roles or other theaters was toast as an interceptor/air superiority fighter over NW Europe by the end of 1941.
 
My brother often points out that Gloster went from the Gladiator to the Meteor. They did other designs in betwee,n but none that I can think of entered serious production.
From 1934 Gloster was part of Hawker Aviation They produced Hurricanes and Typhoons as a sub contractor and developed the Gloster "Whittle" and Meteor Jets.
 
 
 
This doesn't really count because we are not talking about
the P-51H. Which from what I have read actually flew a few
sorties during WW2, no actual firing its guns though.
Sandard Aircraft Characteristics 22 March 1949.
Interceptor Mode (8,740 lb.): 473 mph./22,700 ft.
Initial rate of climb: 5,480 fpm.
At 9,585 lb. climb to 25,000 ft./6.7 minutes.
At 8,740 lb.: ?, Jeff
 

This graph has been graciously given to the public by Mr. Mike Williams.

Clayton, I have not seen any climb graph of the Spit 14 being tested at +21 lb.
The Spitfire MK.XIV was never cleared for +25 lb. boost.
 

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Clayton,
No sir, it is not a typo. The Griffon 65 was tested at +25 lb.
It just was never cleared for combat at that level of boost.
It was an engine failure vs.performance gain kind of thing.

I can tell you this. If Mr. Edgar Brooks was still here, that
good old boy could have explained the reasons why way
better than I will ever be able to.
 
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