Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      24 m2
    • Wingspan (Beam)
      10 m
      15 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
      412 kg
      618 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      664 kg
      996 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
      136 km/h
      206 km/h
    • Сruise Speed
      116 km/h
      174 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      84 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
      78 hp
      118 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2880 m
      4320 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      536 km
      804 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
      201 m/min
      303 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
      56 qt
      86 qt
    • Price
      41 USD
      750000000 USD

Albatros L 101

TypeAircraft
Company

Albatros Flugzeugwerke

Scheme

Parasol

Monoplane

Geometry
Length (m)
1.9
 
8.5
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
20
925
Wingspan (Beam) (m)
0.1
 
12.5
95
Weights
Empty weight (kg)
8
 
515
276,800
Loaded weight (kg)
5
 
830
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
171
28,165
Сruise Speed (km/h)
52
 
145
3,087
Landing Speed (km/h)
68
 
70
270
Power
Total Power (hp)
0.4
 
98
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,600
161,544
Range (Ferry range) (km)
4
 
670
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
252
36,000
Stat
Number built (qt)
0
 
71
43,000
Introduction 1930
First flight 1930

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