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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      5 m2
      9 m2
    • Wingspan (Beam)
      8 m
      13 m
    • Wing loading
      21 kg/m2
      32 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
      2 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
      360 kg
      540 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      528 kg
      792 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      3 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      100 km/h
      150 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      84 km/h
      126 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
      40 l
      60 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      44 hp
      66 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 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
      9 min
      15 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      3 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Albatros L.71

TypeAircraft
Company

Albatros Flugzeugwerke

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.2
88.7
Wings
Wing area (m2)
1.1
 
25
925
1.1
 
7.5
925
lower
Wingspan (Beam) (m)
0.1
 
10.1
95
upper
Wing loading (kg/m2)
3.1
 
26.3
829
Rotors
Rotor number (qt)
1
 
1
8
Weights
Empty weight (kg)
8
 
450
276,800
Loaded weight (kg)
5
 
660
242,500
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
2
400
Speeds
Ground Speed (km/h)
96.6
 
125
1,500
Сruise Speed (km/h)
52
 
105
3,087
Fuel
Fuel Capacity (l)
23
 
50
320,000
Power
Power/mass (hp/kg)
0.0
 
0.1
22.1
Total Power (hp)
0.4
 
55
60,000
1 powerplant
Dynamic Performance
Time to altitude (min)
0.6
 
12
105
to 1000 m
Propellers
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
2
43,000
Introduction 1925
First flight 1925

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