CORSNING
Tech Sergeant
WOW! BiffF15 and silence. You guys are really making the rest of us think hard. Excellent posts, both of you. I guess I have nothing to add to the angles you are coming from. Thank you both for that kind of insight. Silence, I owned a 1983 280 ZX "cop come get me red" so I can relate to that exact point you were making. I own a Del Sol now. It actually turns slightly tighter, BUT it doesn't give you that fealing of confidence in handling that the 280 did. So the 280 could be driven right up to its limits with ease. In the 3 dimentional sky that would be a great advantage.
I would like to clarify the dry numbers of the potential of the fighters being compared. All the information I have on these come from the Kurfurst and wwiiaircraftperformance.org sights. Except the Fw190/Ta 152 info came from the graphs in Dietmar's "Longnose" and "Ta 152".
The numbers are altitude in meters, speed in mph and climb in fpm.
Meters..Bf.109K-4---Spitfire 14---Fw190D-9----P-51B-15----Tempest V--Ta152
S.L.......378/4830----370/5080----380/4428----388/4330----404/4380----372
.1,000..397/4840----386/5035----392/4388----404/4220----417/3860----384
.2,000..411/4645----401/4985----404/4124----418/3870----411/3340----396
.3,000..420/4440----417/4485----409/4103----420/3840----411/3000----397
.4,000..428/4235----416/4095----419/3985----420/3770----410/2603----410
.5,000..437/4035----418/4070----429/3493----430/3590----426/2151----422
.6,000..446/3445----432/4025----429/2991----441/3100----436/1705----436
.7,000..442/2950----445/3510----422/2499----442/2620----431/1242----448
.8,000..438/2450----447/2960----416/1987----436/2125----428/.-806----451
.9,000..432/1940----444/2400----406/1485----430/1675----N.G./N.G.----464
10,000.422/1435----437/1875----394/.-984----421/1200----N.G./N.G.----458
11,000.409/.-945----427/1350----NG./-482----411/.-715----N.G./N.G.----448
12,000.390/.-440----414/.-825----NG./NG.-----393/.-245----N.G./N.G.----434
Wt.-----7,497 lbs.----7,923 lbs.---9,591.75 lbs.--9,680 lbs.(9,335 lbs.speed trials)-11,490 lbs. Weight at take-off.
W.L.:-----43.25--------32.73--------48.67---------40.06--------38.04+Wing Loading at take-off ( lbs./sq.ft.).
P.L.:------4.052+------3.569--------4.631+-------4.885---------5.223-Power loading at take-off weight and max. power output
(lbs./hp.)
Power:-1,850hp./1.8ata-2,220hp./+21 psi.-2,071hp./1.8ata-1,910hp./75"Hg.-2,200hp./+11 psi.
Engines: DB 605D---Griffon 65-----Jumo 213A----V-1650-7---Sabre IIA
For more Ta 152 information see POST #864.
I would like to clarify the dry numbers of the potential of the fighters being compared. All the information I have on these come from the Kurfurst and wwiiaircraftperformance.org sights. Except the Fw190/Ta 152 info came from the graphs in Dietmar's "Longnose" and "Ta 152".
The numbers are altitude in meters, speed in mph and climb in fpm.
Meters..Bf.109K-4---Spitfire 14---Fw190D-9----P-51B-15----Tempest V--Ta152
S.L.......378/4830----370/5080----380/4428----388/4330----404/4380----372
.1,000..397/4840----386/5035----392/4388----404/4220----417/3860----384
.2,000..411/4645----401/4985----404/4124----418/3870----411/3340----396
.3,000..420/4440----417/4485----409/4103----420/3840----411/3000----397
.4,000..428/4235----416/4095----419/3985----420/3770----410/2603----410
.5,000..437/4035----418/4070----429/3493----430/3590----426/2151----422
.6,000..446/3445----432/4025----429/2991----441/3100----436/1705----436
.7,000..442/2950----445/3510----422/2499----442/2620----431/1242----448
.8,000..438/2450----447/2960----416/1987----436/2125----428/.-806----451
.9,000..432/1940----444/2400----406/1485----430/1675----N.G./N.G.----464
10,000.422/1435----437/1875----394/.-984----421/1200----N.G./N.G.----458
11,000.409/.-945----427/1350----NG./-482----411/.-715----N.G./N.G.----448
12,000.390/.-440----414/.-825----NG./NG.-----393/.-245----N.G./N.G.----434
Wt.-----7,497 lbs.----7,923 lbs.---9,591.75 lbs.--9,680 lbs.(9,335 lbs.speed trials)-11,490 lbs. Weight at take-off.
W.L.:-----43.25--------32.73--------48.67---------40.06--------38.04+Wing Loading at take-off ( lbs./sq.ft.).
P.L.:------4.052+------3.569--------4.631+-------4.885---------5.223-Power loading at take-off weight and max. power output
(lbs./hp.)
Power:-1,850hp./1.8ata-2,220hp./+21 psi.-2,071hp./1.8ata-1,910hp./75"Hg.-2,200hp./+11 psi.
Engines: DB 605D---Griffon 65-----Jumo 213A----V-1650-7---Sabre IIA
For more Ta 152 information see POST #864.
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