Search filter

    • Year
      1906
      2018
    • Length
      5 m
      8 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      19 m2
      30 m2
    • Wingspan (Beam)
      8 m
      13 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
      520 kg
      780 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      760 kg
      1140 kg
    • Crew
      1 per.
      3 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
      112 km/h
      168 km/h
    • Сruise Speed
      88 km/h
      132 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
      88 hp
      132 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3360 m
      5040 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      288 km
      432 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
      67 m/min
      101 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
      1 qt
      18 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
      14 qt
      22 qt
    • Price
      41 USD
      750000000 USD

Albatros L 68

TypeAircraft
Company

Albatros Flugzeugwerke

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.3
88.7
Height (m)
0.6
 
2.6
50.1
Wings
Wing area (m2)
1.1
 
24.4
925
Wingspan (Beam) (m)
0.1
 
10.1
95
Weights
Empty weight (kg)
8
 
650
276,800
Loaded weight (kg)
5
 
950
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and instructor
Speeds
Max. Speed (km/h)
25
 
140
28,165
Сruise Speed (km/h)
52
 
110
3,087
Power
Total Power (hp)
0.4
 
110
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,200
161,544
Range (Ferry range) (km)
4
 
360
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
84
36,000
Stat
Number built (qt)
0
 
18
43,000
Introduction 1925

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