Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules
.The high performance of the Ta 152 have some caveats, though. The 730-750 km/h figures were to be for the aircraft with half of fuel aboard (only fuselage fuel tanks filled? 525L?), ie. at 4750 kg light 152H instead of 5220 kg, no ETC rack, and with use of MW 50.
We know that weight does slow aircraft - how much the Ta 152?
The ETC will cost a bit - close to 10 km/h?
According to the only power chart of the Jumo 213E that I'm aware, the use of MW 50 system was limited to the lower 2 supercharger gears, meaning that max speed will be attained without MW 50. That would be, still with half of fuel and ETC, 720 km/h at 10,7 km ( 447 mph at 35100 ft); still impressive for that altitude, but how much with full fuel and ETC?
The heavy brute P-47N with 2100 L of fuel aboard (16700 lbs test weight) was doing ~460 mph at 32-33000 ft, the P-47M was still a bit faster.
.
The Serial produced Jumo 213E-1 would have solved ( at least that was the intention) the problems with the 3rd supercharger gear
Brown Reports a speed of 684km/h at 10670m , no GM1, propably not third gear in, power setting unknown
Do you know any aircraft that its maximum speed was calculated at maximum take off weight?
At 4750kgr ,"light" as you mention, the Ta 152H still had 595ltr lt of fuel, 70 ltr more than the entire Internal fuel capacity of the Fw 190A8 ! And the Ta had the option to use its wing tanks for another 400ltr if needed. Do you believe that with such Internal fuel capacity, would be nessecary to have the ETC rack?
The P47M/N had absolutely superb performance at 33000 ft . But i believe the ta with Jumo 213EB and GM1, or at least 213E-1 ,C3 fuel and GM1 could reach such speeds. And it had the advantages of the pressurized cocpit , automatic engine controls and lower wing loading
Biff 15Dedalos,
I didn't read Greg's posts as being as negative as you did.
Also realize that there are at least two versions of Willi's story of how his wingman went down. We discussed this in a previous thread at length. Here is a link to the thread: http://www.ww2aircraft.net/forum/av...e-vs-fw-190-vs-51-a-13369-62.html#post1072052.
I would suggest you read post 926 on page 62, 956 and page 64, and 961 on page 65. There is what I would call strong circumstantial evidence (high quality for the time) that his wingman was shot down and didn't just "crash".
I also think Germany did well producing anything, let alone aircraft especially during the final year of the war. Yes, they did make what I would call a very good airplane in the Ta152 however it's true combat credentials are questionable due to the few (43) that actually showed up. How many it would take to be credible is a number that probably won't ever be identified, however I think Greg's point is 43 isn't enough. I agree. Going past the a/c numbers into it's combat record one person deciding that two of the four shot down don't count, and that the other two were combat accidents could be to another 4 that were shot down or lost due to combat. Or, combat losses. To re-type an oft quoted line among fighter pilots, "A kill is a kill". Also if the two losses from the ferry flight had scored kills, would you count them? If you venture into the arena you are part of the game, whether you want to be or not.
The reason the F8F, P51H, and P80 have no combat record is they were not built under another nations or forces air superiority. When you live under another military's umbrella, you have to deal with that, and the result is an un-vetted or un-sorted aircraft might end up in combat before the bugs are worked out.
Be aware that a person who is very pro one nationality, or type of aircraft, might cast a shadow on their credibility or ability to sort the truth from the fiction.
Cheers,
Biff
but i am sorry but from what i have read both the F8F and P51H were structuraly suspect. They were very good at their very specific missions but not good for all around work. The americans, knew very well that and kept them away from combat
Probably it would.
Goes without saying that I'd gladly take a peek in the original Brown's report.
Not at the maximum take off weight - that would mean, for the fighters, the drop tanks are also carried. But there is plenty of data for the fighters in clean condition, but with maximum fuel aboard, like the example I've gave for the P-47N.
The Fw-901A-8 carried, in most of the cases, 640 L of fuel, due to the installation of the rear fuselage 'drum' tank.
As for whether is necessary to carry the full fuel and ETC in the same time - we need a level play field, if a fair comparison is to be drawn. We can easily find the data for the Allied fighters with full internal fuel and rack(s), but not for the late war Fw fighters.
If it carried the 115 ltr fuselage tank could not Carry MW50 which was preffered in 1945 from c3 injection. But even using c3 injection, meant much more fuel consuption and the additional 115 ltr help little in range.
While the C series of the R-2800 have had it's share of teething troubles, it was in volume production before 1945 started, and was even powering, though in experimental form, a late 1943 XP-47J to 500 mph. By that time (late 1944), the Jumo 213EB was still on test benches? Granted, it would provide the Ta-152 with extra performance, at least by looking at the charts. BTW, the speed figures for the P-47N and M are for the 130 grade fuel, how much faster with 150 grade? And again, how fast the Ta-152 would be with full fuel load and ETC?
The P-47M/N were about as capable as the Ta-152, but the Ta-152 was unable to do what the P-47N was able, namely to provide the combat radius (not range) in excess of 1000 miles. table
Please tell us your source for this?!? The only reason why the F8F wasn't used in combat (Korea) by US forces was because there were other recips readily avilable to be deployed overseas that were more capable, especially in an air to ground mission. By the time the F8F could have been used in a shooting war, it was already eclipsed by jets, let alone assigned to reserve units.
The French operated 200 F8Fs in Vietnam before they left, never heard any reports by them staing the aircraft was "structually suspect." I'll let other chime in on the P-51H...
If the Ta-152H was at low altitude, I suspect the P-47Ms could deal with them sufficiently. P-47Ms appear to be slightly faster, and had an advantage in climb rate as well. At least a 500fpm advantage at sea level, and probably more up to about 30,000'. Above that, I think the Ta-152 would have the advantage in speed and climb. To illustrate its climb, the P-51H climbed to 25K in 6.7 minutes, and the P-47M climbed to 25K in about 7.1 minutes. Information taken from wwIIaircraftperformance SAC charts.
If it carried the 115 ltr fuselage tank could not Carry MW50 which was preffered in 1945 from c3 injection. But even using c3 injection, meant much more fuel consuption and the additional 115 ltr help little in range.
I disagree that P47 M/N were as capable as Ta 152H.It had better range and dive. If the ta had c3 fuel and GM1 had similar level speeds at over 10000m
The ta was much more manouverable.Lowere wing loading. It had pressurised cocpit so could enter combat at higher altitude. Lower pilot work load. If the combat last and height is lost the Ta eventually gets power loading edge as well. In medium / low level ta is clearly superior.
Was possible to use 150 octane fuel on c series 2800s? They were already hard pushed. And P47N was a big plane. It needed important additional power to see notable speed gain.
Finally if you want to compare apples to apples and oranges to oranges if you allow 150 octane fuel for the P47 you should allow 213EB for the ta. Besides what you are meaning c series was in production before 1945? P47M s in england were grounded until march 45 due to engine problems. And had huge fuel consuption that limited their endurance. By that time DB603L (2400 ps) also was ready for production
If the Ta-152H was at low altitude, I suspect the P-47Ms could deal with them sufficiently. P-47Ms appear to be slightly faster, and had an advantage in climb rate as well. At least a 500fpm advantage at sea level, and probably more up to about 30,000'. Above that, I think the Ta-152 would have the advantage in speed and climb. To illustrate its climb, the P-51H climbed to 25K in 6.7 minutes, and the P-47M climbed to 25K in about 7.1 minutes. Information taken from wwIIaircraftperformance SAC charts.
I have a Fw performance table that says for the Ta 152H-0 ,at 4730 kgr, NO MW50, B4 fuel, initial climb rate 20 m/sec, 8 minutes to 7000 m
Unknown power setting
I can certainly agree about the skies of Europe being a target rich environment!Grau,
While I have read Ditmars book on the Ta-152 I don't have it handy for reference. If only 43 were delivered, and were flown only by experten, and achieved only 10 kills in a sky that would have been full of adversaries, and lost 3-4 of their own it does open a quandary...
Was possible to use 150 octane fuel on c series 2800s? They were already hard pushed. And P47N was a big plane. It needed important additional power to see notable speed gain. Finally if you want to compare apples to apples and oranges to oranges if you allow 150 octane fuel for the P47 you should allow 213EB for the ta. Besides what you are meaning c series was in production before 1945? P47M s in england were grounded until march 45 due to engine problems. And had huge fuel consuption that limited their endurance. By that time DB603L (2400 ps) also was ready for production [/B]
[I'll politely ask you to provide credible sources on the BMW 801 ever using the MW 50 system. The 190A-8 never used the C3 injection, but the 'simple' overboost (with about the same increase of manifold pressure and, hence, power).
For the P-47M/N, we don't have any 'ifs', apart from possible use of 150 grade fuel. The 'ifs' for the Ta-152 are numerous - GM1, clearance for MW 50 usage in 3rd supercharger speed, experimental engines, 'zellenfeste werkleidung' etc.
The P-47N have had the rear-warning radar and anti-G suits available before the ww2 ended, not the case for the Ta-152.
As for the capabilities - I've posted a number of performance figures for the P-47M/N with full internal load, so I expect the same for the Ta-152. Not to be impolite, just that I cannot locate any.
GM1 operation, mw 50operation , were not ifs, were just minot teething problems that took longer to be solved because it was raining bombs. Several of the "experimental engines" were ready, were not produced due to the unavailability of C3 fuel. Tell me how the r2800c would perform with 92 octane fuel?
The Ta-152 will be killed from attacks in rear hemisphere, since we know that 3/4 of fighters were disposed that way, unknowingly to their pilots - it carries no tail-warning radar. Failing that, it will not be able to roll as good as the P-47. It will not do well in sustained high-G turns, since the pilot will black out. Unlike the P-47, it will succumb to any late-war gun burst that hits.
The Ta would patrol at 12-13000 m with its pressurized cocpit. Could P 47 pilots Cruise at that altitude?How will surprise the Ta? . Also they would be no sustained turns. The ta would quiqly out turn/outmanouver the P47. What about wing loading and power loading? Accelaration? Responce of the engine to power changes? Wing profile? Support with data your thesis that the p47 will outroll the ta152
The Ta 152 with its 150kgr of armor and the proven strong fuselage of the a8 will succumb to the 12,7mm guns while the P47 would withstand 2x20mm,installed Near the central axis of the aircraft, firing the best ammo of the war PLUS the 30mm Mk 108 cannon which alone was bringing down B 17s??????. You seriously believe this??????
The ta has 15 mm armor around its radiator. Tell any other fighter with in Line engine which protects its radiator better. 20mm head armor
The fw family had iclined Seat. A design future of the aircraft. The g suit was not design future of any aircraft. And an idea very easily to be copied
Would the P47 pilot be able to keep the engine at optimum tuning during sustained combat? The ta 152 pilot had not such problems
Don't know whether the 150 grade was used on the R 2800 C. The high power was put in a good use with P-47s.
[
[/B]I mean exactly as I've wrote - the R 2800 C were in series production prior 1945, and yes, I've noted they have had issues. That is still far bigger asset than the 213EB, that never flew in an operative aircraft.
Yes , P&W and junkers had the same working conditions
The combat radius of the P-47M was 400 miles, with 370 gals of internal fuel and only one, 110 gal tank under centreline. How much with 2 x 165 gal tanks instead of that drop tank?
The P-47N was the only single engine fighter to have 1000+ miles (or 1310, by the table in the above post, probably on relaxed cruise settings) combat radius. That is because the R 2800 was on board, not despite.
GM1 operation, mw 50operation , were not ifs, were just minot teething problems that took longer to be solved because it was raining bombs. Several of the "experimental engines" were ready, were not produced due to the unavailability of C3 fuel. Tell me how the r2800c would perform with 92 octane fuel?
The Ta would patrol at 12-13000 m with its pressurized cocpit. Could P 47 pilots Cruise at that altitude?How will surprise the Ta? . Also they would be no sustained turns. The ta would quiqly out turn/outmanouver the P47. What about wing loading and power loading? Accelaration? Responce of the engine to power changes? Wing profile? Support with data your thesis that the p47 will outroll the ta152
The Ta 152 with its 150kgr of armor and the proven strong fuselage of the a8 will succumb to the 12,7mm guns while the P47 would withstand 2x20mm,installed Near the central axis of the aircraft, firing the best ammo of the war PLUS the 30mm Mk 108 cannon which alone was bringing down B 17s??????. You seriously believe this??????
The ta has 15 mm armor around its radiator. Tell any other fighter with in Line engine which protects its radiator better. 20mm head armor
The fw family had iclined Seat. A design future of the aircraft. The g suit was not design future of any aircraft. And an idea very easily to be copied
Would the P47 pilot be able to keep the engine at optimum tuning during sustained combat? The ta 152 pilot had not such problems
Yes , P&W and junkers had the same working conditions
Did i ever said that P47N was not Top class fighter? It had its strong points and its weaknesses. Better escort fighter than the Ta 152 worse ,as General Air superiority fighter
F8F in action. Squadron/signal publications. Page 14. The F8f had the unique design charachteristic of broken wingtips. There were several occasions that f8f lost their wingtips. Especially during strafing and bombing exercises. Unfortunately there was at least one fatality. In 1947 the American navy was forced to rebuilt the wings.
For the P51H sveral sources. Now, immediately joe bauer page comes to my mind