We all know about the Spitfire being used for high altitude interception of JU86P(I think) at 49,000 feet. The P47 was also very good at high altitude, one of, if not the best high altitude fighter of WW2.
Could a P47 have made the 49,000 foot interception? I know it would have to be lightened, so lets ditch 6 of the 8 machine guns and all of the armor plate to make it a special, high altitude PR interceptor.
Was the P47 capable of doing the job?
I would tend to check the accuracy of these kinds of claims. There are lots of reports that once subject to post war analysis don't pan out. The stories of modified Spifire V or VI intercepting Ju 86R for instance turn out to be false (as do the claims of Sunderlands shooting down 8 x Ju 88, but that's another story). There are claims of a Ju 388L being intercepted at 46000ft over England and then being shot down I can't find any validating reference to the Luftwaffe undertaking these missions let alone the names of pilots on either side.
As far as I can tell the highest "name plated" service ceiling of any operational interceptor was the Focke-Wulf Ta 152H. The aircraft was pressurised, had double walled canopy to stop the stratospheric cold from causing condensation on the inside of the cabin (which could completely blind a pilot). The technology used was the Jumo 213E1 engine which used a two stage three speed supercharger combined with cryogenic nitrous oxide (GM-1) which drove the service ceiling up from about 44500ft to 48500ft. The aircraft was very heavily armed and armoured and I suppose they might have achieved more if they stripped down the aircraft somewhat.
The argument against turbo-superchargers is that they add a lot of bulk, weight and drag, they reduce jet thrust somewhat and for all the extra power generated a larger and heavier propeller is also required. For this and other reasons cryogenic nitrous offered a good solution. The RAF also used it as well as experimenting with pure oxygen.
Without pressurisation there is the possibility of the "bends": nitrogen coming out of solution in the blood and forming bubbles as the aircraft climbed similar to a diver coming up after a long deep dive. A partial solution to that was to breath near pure oxygen during the climb and even before takeoff to let the nitrogen dissolve out of the lungs into the lower partial pressure created by the pure oxygen.
I really don't know how Me 163B rocket pilots did it.
Interesting to me is the 'special diets' some ww2 pilots and crew received to stop the pain caused by gases in the gut expanding. I have never found a menu or a recipe. I imagine all that is required is the avoidance of any wheat based products such as bread, pasta, likely oats as well and beans. Rice does not cause much if any gas, vegetables such as spinach and fennel do not either. Meat, fat and eggs are also OK.
As far as the P-47 goes:
At At 0ft (seal leve), the standard barometric pressure is 101 kPa (760 mmHg).
At At 44000ft (service ceiling), the standard barometric pressure is 17 kPa (131 mmHg).
At 49000ft, the standard barometric pressure is 14 kPa (103 mmHg)
So we've only got 103/131 78% as much air density at 44000ft as at 49000ft and therefore lift.
That would suggest you need to lighten the aircraft by 22%. (100%-78%). Might be possible with guns, armour and of course P-47 tests were probably carried out with near full fuel tank.
I used the following calculator and assume temperature is stable at these altitudes so that pressure and density are proportional.
Altitude.org | Altitude air pressure calculator
critical altitude of the latter turbo R-2800 was about 28000ft (earlier 25000ft) and so there would also be a decline from there, which I assume is approximately linear
At 28000ft, the standard barometric pressure is 35 kPa (264 mmHg) so I'm figuring that at 44000ft power was reduced to 131mmhg/264mmhg 49% (half power)
whereas at 49000ft the power might be 103/264 = 39% (ie there has been a 20% loss from 44000ft to 49000ft). There would also be a reduction in parasitic drag.
If there was a low fuel load, armour removed and most armament reduced, the airframe in good condition it might be possible. Worst case one would have to reduce the weight to 0.78 x 0.8 = 63%, but as I mention, parasitic drag is reduced.
As far as German aircraft high altitude champions that reached prototype stage but didn't get to a first flight: there was to be the Ju 488 with 51000ft with 4 x BMW801TJ (more with the 801TQ) and the Blohm and Voss BV.155 Service ceiling was to be 16,950 m (55,610 ft).
The massive size of the BV.155 intercoolers gives an indication of the technical challenges in compression the air to this degree. The aircraft is an almost unrecognisable Me 109 developed from the Bf 109T (with extended wings for the aircraft carriers) with turbo charging and intercooling added to a new laminar flow wing.
As far as I know the USAAF usually attacked at below 25000ft, where both the Fw 190 and Me 109 still had reasonable performance, but occasionally went higher for heavily defended targets. At 30000ft the principle German FLAK gun, the FLAK 37 was ineffective whereas as the Me 109/Fw 190 were at a big disadvantage unless using cryogenic nitrous oxide with which only a few hundred fighters were equiped. The German 10.5cm and 12.8cm FLAK 38 and FLAK 40 as well as the 8.8cm FLAK 43 were still effective but there was much less of them. Perhaps 15% as many.