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    • Year
      1906
      2018
    • Length
      20 m
      31 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      98 m2
      148 m2
    • Wingspan (Beam)
      27 m
      41 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
      10501 kg
      15753 kg
    • Max. takeoff weight (Gross weight)
      19240 kg
      28860 kg
    • Loaded weight
      17805 kg
      26709 kg
    • Crew
      2 per.
      4 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
      350 km/h
      526 km/h
    • Сruise Speed
      268 km/h
      402 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
      3240 hp
      4860 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5040 m
      7560 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5280 km
      7920 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      3200 km
      4800 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
      600 m/min
      900 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
      2 qt
      4 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      12 qt
      18 qt
    • Price
      41 USD
      750000000 USD

Junkers Ju 252

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
25.1
88.7
Height (m)
0.6
 
5.8
50.1
Wings
Wing area (m2)
1.1
 
122.6
925
Wingspan (Beam) (m)
0.1
 
34.1
95
Weights
Empty weight (kg)
8
 
13,127
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
24,050
575,000
Loaded weight (kg)
5
 
22,257
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
438
28,165
Сruise Speed (km/h)
52
 
335
3,087
econ cruise
Power
Total Power (hp)
0.4
 
4,050
60,000
3 powerplants 1350 hp each
Performance
Service ceiling (m)
0.6
 
6,300
161,544
Range (Ferry range) (km)
4
 
3,981
40,700
with maximum payload
4
 
6,600
40,700
with 2000 kg payload
Сombat radius (km)
277
 
4,000
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
750
36,000
Combat
Guns (qt)
1
 
3
18
1 x 13 mm MG 131 machine gun in dorsal turret; 2 x 7.92 mm MG 15 machine guns in side windows
Stat
Number built (qt)
0
 
15
43,000
Introduction 1943
First flight 01.08.1942

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