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2017-11-20

 

Bf109 - Additional Notes/6

Table  -  Bf109G1

E3


 
 

BAUBESCHREIBUNG

fr das

FLUGZEUGMUSTER MESSERSCHMITT ME 109

mit

DAIMLER-BENZ-MOTOR DB 605

 
 
IV/43/42
  Engine (reduction gear) DB 605 (9-605-2008) 1:1,685
  Engine (reduction gear) DB 605 (9-605-2008)
  Startleistung (PS/revs/min)
  Engine output at Sea Level
1475/2800
1310/2600
1230/2600
  Propellor m 3 3 blades.
  Wingspan
  Lenght
  Height
  Wing area
m
m
m
m
9,97
8,94
2,45
16,10
  Armament 2xMG17
1xMG151
2 x 500 rounds
1 x 500 rounds
  Equipped Weight
  Crew          (                  ....  Mann)
  Ammunition (2 MG 17 /1 MG 151 Schu)
  Fuel
  Lubricant
  Bombs
  Flying weight
kg
kg
kg
kg
kg
kg
kg
2546
  100
   73
  296
   27
   ---
 3042
  Maximum Level Speed N(PS) H(km)
1230 V H (7,0 km) km/h 660
1270
1350
1350
1260
860
0
2
4
6
10
km/h
km/h
km/h
km/h
km/h
535
583
624
647
638
  Cruising speed and range
  at max.continous output, middle weight 2780kg
N(PS) gbr (gr/PS/h)
1090 225 0
2
4
6
-
-
-
600 km/h
  Endurance at 6 km with economy continous. h 1,1'
  Service ceiling at Ga*
  Service ceiling at Gmittel
  Service middle ceiling w. 1 engine Ga*
km
km
km
12,2
  Climb time at Ga* H = 1 km
                        2
                        4
                        6
                        8
min
min
min
min
min
0,9
1,8
3,6
5,7
8,5
  Landing speed at weight = 2740 kg
  (w/o.Bombs, with fuel for 2/3 h Vm)
km/h 140
  Wingloading kg/m 180

corresponds to Rechlin guidelines from 26 August 1939  -  Augsburg, den 17.5.42