Search filter

    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      51 m2
      78 m2
    • Wingspan (Beam)
      18 m
      28 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
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      16800 kg
      25200 kg
    • Loaded weight
      16760 kg
      25140 kg
    • Crew
      3 per.
      5 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
      496 km/h
      744 km/h
    • Сruise Speed
      52 km/h
      3087 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
      4260 hp
      6392 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7440 m
      11160 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2160 km
      3240 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      2880 km
      4320 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
      348 m/min
      522 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
      6 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2400 kg
      3600 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      17 qt
      27 qt
    • Price
      41 USD
      750000000 USD

Junkers Ju 288

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
17.8
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
64.6
925
Wingspan (Beam) (m)
0.1
 
22.7
95
Weights
Max. takeoff weight (Gross weight) (kg)
154
 
21,000
575,000
Loaded weight (kg)
5
 
20,950
242,500
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
620
28,165
Power
Total Power (hp)
0.4
 
5,326
60,000
2 powerplants 2663 hp each
Performance
Service ceiling (m)
0.6
 
9,300
161,544
Range (Ferry range) (km)
4
 
2,700
40,700
Сombat radius (km)
277
 
3,600
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
435
36,000
Combat
Guns (qt)
1
 
5
18
4 × 13 mm (.51 in) MG 131 machine guns; 1 × 15 mm (.59 in) MG 151 cannon or 20 mm MG 151/20 cannon
Bombs weight (kg)
2
 
3,000
39,000
Stat
Number built (qt)
0
 
22
43,000
Introduction 1941
First flight 29.11.1940

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