Originally posted by Karnak
EDIT:
The P-38 as described by Captain Virgil Hilts (derived from reading his posts on the subject):
450+mph
4,500fpm+ climb
no compression issue (myth made up by a corrupt congressional comitee)
Rolls faster than an Fw190
Turns better than a Spitfire Mk V
Longer ranged than a P-51D
More durable than an Il-2
Easier to fly than an A6M2
100% viceless and impossible to stall (twin engines will do that you know)
The perfect prop fighter.
Karnak, if you'd like to make this really nasty, I can certainly accomodate you. If you'd like to continue to make up lies for quotes from me and take them out of context, I can deal with that as well.
Here is the truth about what I've posted, taken directly from data I keep handy:
The following are the CORRECT stats for the Allison V-1710F-30. Write 'em down somewhere....
Ratings [minutes] Power RPM Manifold [in.Hg] Altitude [ft]
Normal (no limit) 1,100 2,600 44 30,000
Take Off (5) 1,475 3,000 54 SL
Military (15) 1,475 3,000 54 30,000
WEP (5) 1,725 3,000 60 28,700
The most commonly printed max speed numbers for the P-38L state 414 mph. How interesting. Consider that the L was fitted with the -30 Allisons, as opposed to the -17 on the J. There is a big difference, and I'll go into that a little later. The typical numbers presented for the J are 421 mph IN WEP. The typical numbers presented for the L are 414 mph IN METO. This is one of the pitfalls of using commercially available data. It usually isn't researched very well. The difference between METO and WEP is 600 hp. The -30 produced a minimum of 1,725 hp in WEP. As opposed to 1,425 hp in METO. The -17 installed in the P-38J had the same METO rating as the -30 at 1,425 hp. However, the -17 only made 1,600 hp in WEP. The additional power could push the L to speeds over 440 mph. Warren Bodie concludes the maximum speed in WEP as 443 mph at altitudes between 20,000 and 23,500 ft. Bodie obtained his data directly from Lockheed, where he was employed as an engineer on the U-2 and F-117 programs.
Max climb rate at sea level: 4,225 fpm (50% fuel, normal ammo) Max climb rate at 23,400 ft: 3,940 fpm Time to 23,400 ft: 5.94 minutes Time to 30,000 ft: 8.86 minutes Service Ceiling: 44,000 ft.
The basic performance figures for the P-38L are as follows (from Lockheed factory test logbooks): Max speed at sea level: 352 mph Max speed at 5,500 ft : 369 mph Max speed at 23,500 ft. 440 mph (WEP) 5 minutes max. Max speed at critical alt: 444 mph @ 25,800 (WEP) 5 minutes max.
Now, nowhere did I EVER say the P-38 did not suffer from the effects of compression. I said that no less than a dozen well know and often quoted P-38 pilots, some of whom I still correspond with on a semi regular basis said this: "After the introduction of the dive flaps, it was no problem to roll over and follow an enemy plane down from 25,000 feet, before the dive flaps you'd compress. Below 20,000 feet you could follow the enemy down without undue drama, even without the dive flaps."
I said that at high speed the P-38J-25-Lo and later rolls faster than a P-51, and approaches the roll rate of the FW 190 and the P-47. Note I said approaches, not exceeds.
Never did I say the P-38 could out turn a Spitfire. I did say that some P-38 pilots were able to turn with some Spitfire pilots, at some speeds and in some cases.
The P-38J with leading edge wing tanks and drop tanks flown at the proper throttle settings does have more range than a P-51D.
I've NEVER compared the P-38 to an IL2 in any way. I did say that the P-38 was only exceeded in durability by the P-47.
I never said it was easier to fly than a Zero.
I never said it would not stall, nor that it would not ever spin. I said it had a very gentle stall, and was not prone to spins. I never said the P-38 was without vices.
You sir, are a fool and a liar, and an ankle humping loser as well.
As I said, if you want to get nasty, and you want to misquote me, or take my statements out of context, or just plain lie like the scum you are, I can deal with that as well. Bring it on little man, keep it up and you'll be glad the HTC staff will put a stop to this.