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Originally Posted by wmaxt The P-38 (not even an L) took on a Spit XIV (Griffon engine) and took the match. |
I'd like to know where I can see this test, urban myth, or whatever it is.
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Originally Posted by wmaxt Go to the Pro Docs page and there is a test of a Spit IX and P-38F. |
I did, and whats so special about it ?
All I see is a very lightly loaded P-38 being slightly behind an early version Spitfire IX in climb.
The weight of the P-38F in question is only 15,000 lbs fully loaded, thats a wing-loading of just 45.8 lbs/sq.ft, now when you add the fowler-flaps at slow speed thats a very low lift-loading for such a big aircraft.
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Krazi,
What is it with you ? Are you just looking for a fight or what ? I mean why else would you bring the Spitfire into this discussion ??
But ok, I'll take the bate then...
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Originally Posted by KraziKanuK The only K-4 that had a high climb rate was the one that was boosted to 1.98ata and these only showed in very small numbers from mid March 1945. Of some ~140 onhand in early April, only ~70 were operational. (50%) |
142 were on hand, and 79 were serviceable.
Anyway please let us know how many Spit XIV's and IX's were running at 21-25lb boost by comparison then. Or better yet let us know how many Spit XIV's were on hand in total, regardless of what boost they used ?
Also perhaps you have forgotten that the 109K-4 was allowed to run at full boost for 10min at a time, where-as the Spit XIV and IX were only allowed to run at full boost for 5min ?
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Originally Posted by KraziKanuK At 1.80ata it was slower (RoC) than the 25lb boost Spit IXs and 21lb boost Spit XIVs. |
If you go by Mike Williams figures for an overweight K-4 which is equipped with gun-pods and therefore not only exhibits more drag that usual, but is also alot heavier than usual - then yeah sure, eventhough at 1.8ata it still climbs at 4,400 ft/min with that setup. I'd like to see how a Spit XIV equipped with a 300L drop tank climbs compared to that
But to give you abit of an Idea of how fast a "clean" Bf-109K-4 would be climbing, please note this:
Bf-109K-4 Power-loading at 1.8ata (1,850 HP): 1.8 kg/hp
Bf-109G-2 Power-loading at 1.3ata (1,475 HP): 2.1 kg/hp
Bf-109G-2 climb rate at 1.3ata - 24 m/sec (4,724 ft/min):
So we can expect a cleanly loaded K-4 flying at 1.8ata boost to be climbing at over 5,000 ft/min, not bad huh ? Makes one wonder how fast it was at 1.98ata doesn't it ?
Not convinced ? Take a look at the HA-1112-MIL Buchon then, it has a slightly higher wing-loading than the G-2, but its power-loading is pretty low:
Loaded weight: 3,180 kg
Engine power: 1610 HP
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Power-loading = 1.9 kg/hp
Max Climb rate: 5,580 ft/min.
Franz Stigler, German fighter ace: "The K-4 was very much like the 109G, yet could leave all other fighters behind in climb. " Quote:
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Originally Posted by KraziKanuK You got data to back up your Dora claim? |
And what "claim" would that be ?
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Originally Posted by KraziKanuK Not the data for the few 'specials' either. |
Haha

And what the heck is that supposed to mean, huh ? A moment ago you were talking about 25lb boost Spit IX's and 21lb boost Spit XIV's !
But ok I'll explain why a P-38L/J will never out-climb a Fw-190 Dora-9:
Fw-190D-9 normal loaded weight: 4,270 kg (9,414 lbs)
P-38J lowest Gross weight: 7,937 kg (17,500 lbs)
P-38L lowest Gross weight: 7,937 kg (17,500 lbs)
Fw-190D-9 Wing-loading: 233 kg/m2 (47.7 lbs/sq.ft.)
P-38J Wing-loading: 260 kg/m2 (53.4 lbs/sq.ft.)
P-38L Wing-loading: 260 kg/m2 (53.4 lbs/sq.ft.)
Fw-190D-9 Power-loading: 1.9 kg/hp (4.2 lbs/hp)
P-38J Power-loading: 2.48 kg/hp (5.46 lbs/hp)
P-38L Power-loading: 2.48 kg/hp (5.46 lbs/hp)
This is more than enough proof that the P-38 never even approached the climb rate of the Dora-9, but I bet you aint satisfied yet, so I'll continue;
Fw-190 D-9 climb rate using "Sonder-notleistung" (2,100 PS), with ETC-504 rack - 21 m/sec (4,133 ft/min) :
http://img230.imageshack.us/img230/9339/d9climb8yo.jpg
That ETC-504 belly rack takes away approx. 10-15 km/h of the top speed, so you can pretty much expect it takes about 0.5-1 sec away in climb rate as-well.(I bet thats what that partly erased line reaching 22m/s is supposed to represent) And remember this is only using "Sonder-notleistung" (Special emergency power), with a output of 2,100 PS, but it can do even better than that;
Max level speed and power output using "Sonder-Notleistung mit A Lader als Bodenmoter" (Special emergency w/ Compressor, C3 and MW50), with ETC-504 rack - output = 2,250 PS, 640 km/h at SL:
http://img482.imageshack.us/img482/3...d2chart2cy.jpg http://img482.imageshack.us/img482/6...mo213a10cn.jpg
Without the ETC-504 rack you can expect a top speed at SL of 650-655 km/h, and the climb rate can be expected to be around 23-23.5 m/s (4,500-4,600 ft/min).
Now about the P-38;
According to the Pilots manual the P-38J/L's climb rate at its lowest gross weight of 17,400 lbs is around 3,200 ft/min at 54" manifold pressure. However according to a test with various american fighters(F4U-4,P-51B,P-38J,F4U-1), the P-38J with a 50% fuel load and running at 60" MP could hit ca.3,775 ft/min. Now thats at the high end of what I would expect from the P-38, but considering the weight of the aircraft it sounds plausible. (The F4U-4 climbed at 4,500ft/min in that test btw, now thats smoken !)
From the P-38L pilots manual:
http://img239.imageshack.us/img239/1...clchart2op.jpg
So there you have it, the P-38 could not follow the Fw-190 Dora-9 in a climb, not even when the Dora-9 was flying at its second best power rating and the P-38 at its highest, it simply didn't have the power or the lift necessary.