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    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      10 m
      16 m
    • Wing loading
      43 kg/m2
      65 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      6
      10
    • 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
      624 kg
      936 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      960 kg
      1440 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
      168 km/h
      252 km/h
    • Сruise Speed
      156 km/h
      234 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
      177 l
      267 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
      189 hp
      285 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4000 m
      6000 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
      2 h
      5 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
      235 m/min
      353 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
      8 qt
      12 qt
    • Price
      41 USD
      750000000 USD

Albatros L 102

Company

Albatros Flugzeugwerke

Scheme

Parasol

Monoplane

Geometry
Length (m)
1.9
 
8.8
88.7
Height (m)
0.6
 
3.1
50.1
Wings
Wing area (m2)
1.1
 
22.2
925
Wingspan (Beam) (m)
0.1
 
13.3
95
Wing loading (kg/m2)
3.1
 
54.1
829
Aspect ratio
1.7
 
8.0
25.6
Weights
Empty weight (kg)
8
 
780
276,800
Loaded weight (kg)
5
 
1,200
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
210
28,165
Сruise Speed (km/h)
52
 
195
3,087
Fuel
Fuel Capacity (l)
23
 
222.4
320,000
160 kg
Power
Total Power (hp)
0.4
 
237
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,000
161,544
Endurance (h)
0.0
 
3.5
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
294
36,000
Stat
Number built (qt)
0
 
10
43,000
First flight 01.09.1932

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