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Wheres this data that shows the P-51 doing 375mph @ sea level w/ full arnament load. Just curious.
So it seem like they were probably in pretty decent condition to start with. That flight from Pensacola to Norfolk must have been fun!I talked to my brother and he said that they were responsible for insuring flight qualifying. He stated that much checking out was on the flight from Pensacola to Norfolk. There the planes would be flown by Navy pilots to Israel. He said that as soon as they landed the planes would be loaded with fuel and weapons and Israel pilots would climb in a fly off, presumably on a mission.
The Bf-109K, pulling 1.98atu, approx. 2000 hp, did less than 365 mph, least according to Kurfurst chart below
http://www.kurfurst.org/Performance_tests/109K_PBLeistungen/files/5026-26_DCStart_noMW_geschw.jpg
According to AF test, the P-51D does 375 mph at SL pulling 67"Hg, loaded with full armament load and full wing fuel and 35 gallons in the fuselage tank. This would reflect the flight condition on initial release of drop tanks when engaging Bf-109s over Germany. 67" Hg at sea level equates to 1630 hp.
http://www.wwiiaircraftperformance.org/mustang/p51d-15342-level.jpg
So, the P-51D, with 370 less hp, is faster at SL than the Bf-109K, pulling 1.98atu. Looks like apples to apples to me. And, the Mustang does this with 2200 lbs more weight, a much larger fuselage and 33% larger wing. This is with 67' Hg and, at the time of the Bf-109G-10/K, the P-51D was approved for 75" Hg, or about 1800 hp at SL.
I never claimed the P-51D was better at climb, or a better fighter than the Bf-109G-10 or K, which I don't think it is. I only claim that the P-51D aero integration is vastly superior to any Bf-109 configuration, which should be expected with about six year's difference in design.
Not to mention that the DB 605ASCM was another 2000ps monster.
Hello Juha,Hello Ratsel
So how many 109s there were in front line units with 2000hp engine? All concrete I'm aware was the message that the unit selected for field testing 1,98ata had convereted 11 by 6 March 45, so quite rare bird according to that info.
Juha
Juha,
There is some research there at kurfurst site here: Kurfürst - OKL, GdJ-Grp. Qu-, Br. B. Nr. 1561/45 g.Kdos. von 20. März 1945.
It say: 4 Gruppen at 1,98 atü.
'Remains (at) 1,98 boost pressure increases' is what it says. Regardless, the DB 605ASCM was making 2000ps w/o the required 1,98 ata boost. And it made more ps from sea level to 6000 meters. It was also introduced in October/44. G-6/AS, some Mtt-Reg G-10's had them.
Juha,
There is some research there at kurfurst site here: Kurfürst - OKL, GdJ-Grp. Qu-, Br. B. Nr. 1561/45 g.Kdos. von 20. März 1945.
It say: 4 Gruppen at 1,98 atü.
Look, RLM, IG Farben, everyone else, they specified, use B4 on fighters. We'd rather you used kerosine, but if you have to use B4. C3 really for development only. That's the clear and laid out message I get from reading their stuff. I understand this is real opinionated and please excuse me if I'm being ignorant in some way.
And yet the allies estimated that 2/3 of German aviation fuel production at the end of the war was C3 grade. I can't find the report,it's probably on Kurfurst's sight somewhere. I linked to it,or quoted it in some other thread here.
Cheers
Steve
Really.. where did you get your information on the DB 605ASC(M)? Would be very interested in seeing that.
Kurfürst - DB 605 DB/DC <- shows the 2000ps 1,98 ata engine introduced in 1944.