This
calculated performance sheet was prepeared just a
month before the operational introduction of the Bf 109G, by when
serial
production was already under way. The calculations were acceped as the
official performance specifications for the Bf
109G-1 subtype, as these very figures were repeated as reference values
in a report on the ERLA factory's speed measurements on 13 serial
production aircraft (along with the +/- 3%
tolerance limits, ie. a minimum 640, maximum 680 km/h being the borders
for acceptance by BAL).
Appearantly the calculated dataset proved rather accurate - the avarage of the ERLA values obtained on production airframes was 652 km/h (the accepted airfames results ranged from 632 to 664 km/h, the three rejected airframes below the minimum tolerance not included), and three production airframes exceeding the reference specification; however the avarage the rated altitudes measured (ranging 6450m to 6950m) was lower, 6700m, probably as a result of the greater variance in thermal effiency than expected originally. It should be noted that the ERLA values were obtained with 120 mm wide radiator flap opening, about three times of the usual standard Schnellflugstellung (which was 40mm), resulting in higher drag and must have reduced the obtained speed results slightly. Trials at E-Stelle Rechlin on a Bf 109G-1 - the results were later becoming the official specifications for the type in a Kennblatt issued on 8 March 1943 - resulted in 650 kph at 6400m; the tested aircraft appearantly had a fixed tailwheel resulting 12 km/h speed loss, which needs to be taken account. Soviet performance trials at the NII VVS with a captured Bf 109G-2, Werknummer 14 513 are in remarkably good agreement with the Messerschmitt datasheet below : 666 kph was achieved at 7000m altitude. This aircraft's tailwheel was semi-retractable and thus the results are directly comparable to the Messerschmitt datasheet below. Similiar factory trials as Erla's were performed at the W.N.F. and Messerschmitt Regensburg factories underlined Rechlin's (and thus Erla's as well) values.
All aformentioned trials were done at Steig- und Kampfleistungs, ie. 1,3ata boost and 2600 rpm. This limitation was in force until October 1943, when the full rating, 1,42ata boost and 2600 rpm was cleared for operational use for the DB 605A-1. Given the great similiarity it can be also applied to the similiar G-2, G-3 and G-4 subtype, from which the G-1 only differed in the presence of pressurized cocpit and/or the radio set. |
Messerschmitt A G Augsburg |
Me 109 G - 1. Ausführung |
IV/42/42 |
D a t e n b l a t t Me 109 G 1
Ausführung
errechnete Werte. |
|||||
|
|
IV/43/42 | |||
Motor
(Untersetzung) DB 605
(9-605-2008) Startleistung (PS/U/min) Motorleistung Boden " i.H. mit Stauerhöhung (PS/m/U/min) |
PS " " |
1:1,685 1475/2800 1310/2600 1230/7000/2600 |
z.Zt.gesperrt Steig-u.Kampflstg |
||
Luftschraube |
m | 3
Ø 3 flg. |
|||
Spannweite Lange Höhe Flügelfläche |
m
"
"
m2
|
9,97 8,94 2,45 16,10 |
|||
Bewaffnung
2 MG
17 2 x 500 Schuß 1 MG 151 1 x 500 Schuß |
|||||
Rüstgewicht Besatzung ( .... Mann) Munition (2 MG 17 /1 MG 151 .... Schuß) Kraftstoff Schmierstoff Bomben Fluggewicht |
kg
"
" " " " " |
2546 100 73 296 27 -- 3042 |
|||
Höchtsgeschwindigkeit
(Ga) Steig-u.Kampleistung |
N(PS) |
H(km)
|
|
|
|
1230 |
VH
7,0 km |
km/h " " " " |
660 |
||
1270 1350 1350 1260 860 |
0
2
104 6 |
535 583 624 647 638 |
|||
Reisegeschwind. u. Reichweite (max.zulass.Dau- erleistung, bei Gmittel) 2780 |
N(PS) |
gbr(gr/PSh) |
|||
1090 |
225 |
0 2 4 6 |
600 km/h
|
||
Flugdauer im 6 km mit wirtschl.
Dauerleistung. |
h |
1,1' | |||
Dienstgipfelhöhe Ga Dienstgipfelhöhe Gmittel Dienstmittelhöhe 1 Motor Ga |
km " " |
12,2 | |||
Steigzeit mit Ga H = 1 km 2 4 6 8 |
min " " " " |
0,9 1,8 3,6 5,7 8,5 |
|||
Landegeschwind.mit G = 2740 kg (o.Bomben, mit Br. für 2/3 h Vm Flug m.Dauerleistg. Flächenbelastung |
km/h
kg/m2 |
140 180 |
|||
entspr.Rechliner Richtlinien vom 26.8.39 |
|||||
Augsburg, den 17.5.42 Pa/../... [signed] |