Search filter

    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      17 m
      27 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      235 m2
      353 m2
    • Wingspan (Beam)
      35 m
      53 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      11929 kg
      17895 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      20390 kg
      30586 kg
    • Crew
      8 per.
      12 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      160 km/h
      242 km/h
    • Сruise Speed
      100 km/h
      150 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      23 l
      320000 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      2400 hp
      3600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2320 m
      3480 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      4000 kg
      6000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      4 qt
      8 qt
    • Price
      41 USD
      750000000 USD

Junkers K 51

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
23.2
88.7
Height (m)
0.6
 
22
50.1
Wings
Wing area (m2)
1.1
 
294
925
Wingspan (Beam) (m)
0.1
 
44
95
Weights
Empty weight (kg)
8
 
14,912
276,800
Loaded weight (kg)
5
 
25,488
242,500
Capacity
Crew (per.)
1
 
10
112
Speeds
Max. Speed (km/h)
25
 
201
28,165
Сruise Speed (km/h)
52
 
125
3,087
Power
Total Power (hp)
0.4
 
3,000
60,000
4 powerplants 750 hp each
Performance
Service ceiling (m)
0.6
 
2,900
161,544
Combat
Guns (qt)
1
 
6
18
2× 7.7 mm (.303 in) machine guns in nose; 1× 20 mm cannon on dorsal position; 2× 7.7 mm (.303 in) machine guns in each of two upper wing turrets; 1× 7.7 mm (.303 in) machine gun in each of one lower wing turret
Bombs weight (kg)
2
 
5,000
39,000
carried externally
Stat
Number built (qt)
0
 
6
43,000
Introduction 1931
First flight 1932

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