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German version


Notes

Performance table of Bf 109G with various installations

    The following German performance tables refer to the Bf 109G when configured with various kits to enable it to serve in different operational roles and as fighter-bomber, heavy fighter, short range fighter-recce (G-2/R2) or long range fighter-recce (G-4/R3).

    The datasheet appears to be calculated for the individual configurtions and subtypes on the basis of the avarage performance obtained in earlier trials at the Erla factory with 13 serial production  Bf 109G fighters in early 1943. These avaraged 652 km/h at 6700 m altitude, the same as given in the table below for the G-2/R2 fighter-recce variant, which is the closest configuration in the below list to a clean fighter configuration without additional equipment.

    It should be noted that basis Erla trials were performed with the radiator flaps were considerably more opened than the standard 'Schnellflugstellung', ie. 120 mm wide open compared to the standard of 40-50 mm. This would result in an apprx. 12 km/h lower speed compared to the standard way of measuring maximum level speed.

    It is to be kept in mind that all perfomance values noted below refer to the Bf 109G when carrying various extra equipment, i.e.
bomb(s), underwing cannon gondolas or cameras. The performance figures of the so configured subtypes due to the added weight and drag resulted in performance loss compared to the clean Bf 109G, configured for air superiority fighter role.

    The magnitude of performance loss in maximum level speed and added weight (effecting chiefly the rate of climb and ceiling) resulting from extra equipment is given by Leistungzusammenstellung Me 109G for bombs and gondolas and droptanks as the following. The values were understood as at Sea Level :

Fromr two underwing 2cm MG 151/20 cannons in aerodynamic fairings ('Gondelwaffen'), installed complete with amunition :    
- 8 kph loss in speed, additonal 215 kg for take off weight.

From 1 x 250 kg bomb, fitted under the fuselage on a ETC 501 IX b bombrack (inc. loss from bomb rack):
- 40 kph loss in speed, additonal 280 kg for take off weight.

For 4 x 50 kg bombs, fitted in pairs behind each other under the fuselage on a ETC 50 bombrack (inc. loss from bomb rack):
- 24 kph loss in speed, additonal 240 kg for take off weight.

For two 300 liter droptanks, fitted under the wings, as used on limited production long range fighter-recce aircraft (G-4/R3) :
- 26 kph loss in speed, additonal 500 kg for take off weight.
(Note : This value is understood with fairing between the droptank and the racks, while the table's values presumably to a state without these fairings being installed.)

The document does not list losses for the Rb 50/30 camera installation. This was installed in the fuselage behind the cocpit, and a small screening plate was added on the bottom of the fuselage (to keep the camera lenses clean from possible oil leaks from the engine) and added a small amount of drag. The weight of the installation from the clean fighter loading figures appears to be apprx. 80-90 kg.

The above values, used for correction  show good agreement

    The official performance specifications for the G-1 (which applies to the very similiar G-2, G-3 and G-4) at Steig- und Kampfleistung was noted as 537 kph at SL, and 660 kph at 7000m. Take off weight given was 3037 kg (May 1942), while the Leistungzusammenstellung Me 109G report (January 1944) gives it as 3050kg.

An interesting comparison can be made with the G-2/R2 fighter-recce, which is the most comparable configuration to the clean fighter versions, being identical apart from the camera and it's screening plate installation.

The given figures for the G-2/R2 is given below as 523 kph at SL, nd 652 kph at 6700m, which are in very close agreement with :

    For the G-6 (and the pressurized G-5) subtype, the official figures at Steig- und Kampfleistung were noted as 510 kph at SL,
625 or 630 kph at 6600m. Take off  weight was 3100kg. These also show good agreement with

    The date of document is unknown. Considering the production period of noted variants, ie. G-1 (from May 1942)
through G-6 (from February 1943), and the fact that performance is still noted at Steig- und Kampfleistung (1,3ata, 2600U/min for 1310 PS at SL), and not with Start- und Notleistung (which is in turn 1,42ata, 2800U/min for 1475 PS at SL.,This has been cleared for operational in October 1943), it is reasonable to believe the table dates from around mid-1943.

Of particular interest is the notes under the main table, especially the performane gains from the use of GM - 1 boosting.
These values are also confirmed by flight testing in the aformenioned Erla report.






Original


Messerschmitt
A.G.
Augsburg

Flugleistungen Me 109G - Baureihen
Me 109 G
A IV / 260 / 48





Bau-
reihe

Bewaffnung
Bombe, bzw.
Außentank
Bild-
gerät
Gewicht
[kg]
Fläche
[m2]
Geschwindigk.
Steigzeit
auf 6 km
[min]

Steiggeschw.
in 0 km
Dienstgip-
felhöhe
Bemerkungen
Rumpf
Gondel
Höhe 0
[km/h]
Volldruckhöhe
[km/h/km]
G1
2 MG 17, 1 MG 151
2 MG 151
-
-
3260













16,1





512
636/6,6
6,3
17,0
11,7
ohne ETC,
mit Druckkab.


     "                 "
-
4 x 50 kg
-
3290
496
608/6,5
6,5
16,4
11,5


     "                 " -
1 x 250 kg
-
3330
489
595/6,4
6,7
16,1
11,4

G2
     "                 " 2 MG 151

-
3260
512
636/6,6
6,3
17,1
11,7
ohne ETC,
ohne Druckkab.

     "                 " -
4 x 50 kg
-
3270
496
608/6,5
6,4
16,6
11,5


     "                 " -
1 x 250 kg
-
3310
489
595/6,4
6,6
16,3
11,4

G-2/R2
     "                 " -

Rb 50/30
3130
523
652/6,7
5,8
18,2
12,0

G3
     "                 " 2 MG 151
-
3340
511
634/6,6
6,5
16,4
11,5
ohne ETC, mit
Druckkab. FuG16

     "                 " -
4 x 50 kg
-
3370
495
606/6,5
6,8
15,8
11,8


     "                 " -
1 x 250 kg
-
3410
466
593/6,4
6,9
15,8
11,2

G4
     "                 " 2 MG 151
-
3320
511
634/6,6
6,4
16,6
11,5
ohne ETC, ohne
Druckkab. FuG16

     "                 " -
4 x 50 kg
-
3350
495
606/6,5
6,7
16,0
11,3


     "                 " -
1 x 250 kg
-
3390
488
593/6,4
6,6
15,7
11,2

G4/R3
1 MG 151
-
2 x 300 lit.
-
3560
475
562/6,3
7,5
14,4
10,8

G5
2 MG 131, 1 MG 151
2 MG 151
-
3360
502
620/6,3
6,7
16,1
11,4
ohne ETC, mit
Druckkab.ohneGM1

     "                 " 2 MG 151 4 x 50 kg
-
3610
476
563/6,3
7,7
14,1
10,8
   ohneGM1

     "                 "        "
1 x 250 kg
-
3650
469
549/6,2
7,8
13,9
10,6
       "
G6
     "                 "        " -
-
3350
502
620/6,5
6,5
16,5
11,4
ohne ETC, ohne
Druckkab.,ohneGM1

     "                 "        " 4 x 50 kg
-
3560
476
563/6,3
7,4
14,5
10,8
   ohneGM1



1 x 250 kg

3620
469
559/6,2
7,5
14,3
10,6
       "


Beim : Maschinenzustand etspr. heutigem Stand, a.n.
ohne Restabdeckung, MG 131-einbau mit Motorhaubenbeulen, bei G5 bzw. G6 Sporn 1/2 ein.
Geschwindigkeitstoleranz +/- 4 km/h, sämtliche Leistungen mit ,,Steig-Kampfleistung".



Möglichkeiten zur Leistungssteigerung
zellenseitig

Restabdeckungen ca 11-14 km/h
verbesserter MG 131-Einbau, 7-9 km/h
Spornganzein 3-4 km/h
motorseitig

Durch 300 PS GM1 so in 8 km
Höhe, ~30km/h, in 10km ~40km/h
Gipfelhöhemsteigerung ~ 700 m.




          [signed]       17.8.43    [signed]







Last updated 1 February 2007.
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