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The "stripper" P-39 was pretty much down to an airspeed indicator, an altimeter and few engine gauges (to keep from cooking the the engine) also the oxygen system.
Yes, The list is upthread somewhere but here it is again.
We await your response with interest
The gas cockpit heater WAS useless. Specified on the Bell Model 14 (P-400 and P-39D-1/2 EXPORT models) it caused radio static when in use and had an indicator on the instrument panel for when it overheated. Very effective ducted air system used on all the other P-39 models (D/F/K/L/M/N/Q) didn't cause radio static and didn't overheat.
I should have ended it ' We await your response with interest, but not much anticipationMethinks it'll be a long wait. Direct questions haven't been answered with anything other than opinion....and even then, they're ignored more than answered.
It was a great post, but I would have concluded with:I should have ended it ' We await your response with interest, but not much anticipation
There was an operational radar since late March 1942 at Port Moresby. It performed poorly, mainly because inadequate training of its staff, but the fact that there was an operational radar meant that a/c operating in the area needed IFF. More info in this message by late Parsifal SHOULD the P39 have been able to handle the Zero? Was it training or performance?.... The IFF was useless in 1942 NG because there was no accurate radar until fall. The British DID order it but once the P-400s were diverted to NG the IFF would have been removed. To save the weight...
This was a one-off example. I have shown numerous times how a properly equipped 1942 P-39 would have weighed 7150 lbs.Yes, The list is upthread somewhere but here it is again.
This was serial number 41-38291, a P-39D-1. first in standard configuration and then modified.
Removal of the four wing guns and supporting accessories, all of the gear box armor plate, the oxygen system, all radio equipment, all instruments except the altimeter, the airspeed indicator, engine manifold pressure gage, tachometer, temperature and pressure gauges; all tools and fixed equipment not essential for flight at 5,000ft, all ballast and four of the eight self-sealing fuel cells. This saved 1287lbs. On page 159 of "Cobra!" by Birch Mathews.
The only performance figures given are for time to 5,000ft, radius of turn and stalling speed. Time to climb 5,000ft dropped from 2 min 34 sec to 1 min 54 sec.
So they used something heavier? So what is your point? How can you claim the British wanting things that increased weight was perfidy when the US was doing exactly the same. BTW you are doing that thing again where your "never" becomes not "often". Of those 100,000 the P-39s used by the USA as a weapon was also an insignificant amount.One last time, no 30calMGs were used on any AAF/USN P-38E/F/G/H/J/L, P-40D/E/FK/L/M/N, P-47, P-51A/B/C/D, F4F3/4, F4U1/4, F6F, F7F, F8F. None. 100,000 planes, how many used 30cals? None. Except the P-39.
Exactly how many P-40B/Cs actually saw combat with the AAF? How many P-35s? A very insignificant amount.
And how does that look against a P-38, P-47, Mustang I, Spitfire IX, Typhoon? Would you cross the Channel to take on an Fw 190 with it?This was a one-off example. I have shown numerous times how a properly equipped 1942 P-39 would have weighed 7150 lbs.
I would say it would be perfectly reasonable. The Mustang I defied what was known when the Spitfire and Hurricane were designed and ordered.As for the British KNOWING that the 7850lb P-400 with 1150hp engine couldn't go 400mph?
If they knew that they should have told North American to quit fooling around with the NA 73 and just build P-40s.
British tested an 8600lb Mustang I at 370mph with an 1150 hp (?)engine.
Aircobra tested in England was 800lb lighter, used the same engine and was 15mph slower.
Power vs drag determines speed, not power vs weight.
Expecting a smaller, more streamline plane, even if heavier, to make a higher top speed than a larger/older/higher drag airplane was not unreasonable. Difficult but not impossible.
Bell flubbed it, big time.
Your original claim was "Yes the British were still using 30calMGs after the BoB, but the AAF WAS NOT." Again, when shown that you were wrong, your changed your claim, as you always do. 1/5 of USAAC fighters in Philippines on 7 Dec 1941 were P-40Bs (18) and 1/5 P-35s (18), and there were definitely P-40Bs on Oahu.One last time, no 30calMGs were used on any AAF/USN P-38E/F/G/H/J/L, P-40D/E/FK/L/M/N, P-47, P-51A/B/C/D, F4F3/4, F4U1/4, F6F, F7F, F8F. None. 100,000 planes, how many used 30cals? None. Except the P-39.
Exactly how many P-40B/Cs actually saw combat with the AAF? How many P-35s? A very insignificant amount.
Uh... what?One last time, no 30calMGs were used on any AAF/USN P-38E/F/G/H/J/L, P-40D/E/FK/L/M/N, P-47, P-51A/B/C/D, F4F3/4, F4U1/4, F6F, F7F, F8F. None. 100,000 planes, how many used 30cals? None. Except the P-39.
Exactly how many P-40B/Cs actually saw combat with the AAF? How many P-35s? A very insignificant amount.
Lets try again.This was a one-off example. I have shown numerous times how a properly equipped 1942 P-39 would have weighed 7150 lbs.
I wonder why?Bell did show how P-39 weight could be reduced by 1000lbs in May 1943. Details were not provided in the book.
When, oh when, will we get a Brewster Buffalo Expert?
What is being done for the army P-39 needs to be done for the navy's F2A!