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    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      28 m2
      44 m2
    • Wingspan (Beam)
      10 m
      16 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
      1040 kg
      1560 kg
    • Max. takeoff weight (Gross weight)
      1672 kg
      2508 kg
    • Loaded weight
      1600 kg
      2400 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      128 kg
      192 kg
    • Capacity passengers
      3 per.
      5 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      128 km/h
      192 km/h
    • Сruise Speed
      122 km/h
      184 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      90 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
      176 hp
      264 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2480 m
      3720 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
      3 h
      6 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
      2 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
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Albatros L 72

TypeAircraft
Company

Albatros Flugzeugwerke

Scheme

Biplane

Geometry
Length (m)
1.9
 
10.5
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
36
925
Wingspan (Beam) (m)
0.1
 
12.8
95
Weights
Empty weight (kg)
8
 
1,300
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,090
575,000
Loaded weight (kg)
5
 
2,000
242,500
Capacity
Crew (per.)
1
 
1
112
Payload (kg)
23
 
160
122,470
Capacity passengers (per.)
1
 
4
400
or 2 handlers plus 160 kg of newspapers
Speeds
Max. Speed (km/h)
25
 
160
28,165
Сruise Speed (km/h)
52
 
153
3,087
Landing Speed (km/h)
68
 
100
270
with slots closed
68
 
75
270
open
Power
Total Power (hp)
0.4
 
220
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,100
161,544
Endurance (h)
0.0
 
4.5
150
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
4
43,000
Introduction 1926
First flight 1926

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