Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      22 m2
      34 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
      1376 kg
      2064 kg
    • Max. takeoff weight (Gross weight)
      2064 kg
      3096 kg
    • Loaded weight
      5 kg
      242500 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
      176 km/h
      264 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
      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
      480 hp
      720 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
      1 h
      3 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
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      1 qt
      3 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 77v

TypeAircraft
Company

Albatros Flugzeugwerke

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.5
88.7
Height (m)
0.6
 
3.9
50.1
Wings
Wing area (m2)
1.1
 
27.8
925
Wingspan (Beam) (m)
0.1
 
12.8
95
Weights
Empty weight (kg)
8
 
1,720
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,580
575,000
Capacity
Crew (per.)
1
 
2
112
pilot and observer
Speeds
Max. Speed (km/h)
25
 
220
28,165
Сruise Speed (km/h)
52
 
195
3,087
Power
Total Power (hp)
0.4
 
600
60,000
1 powerplant
Performance
Endurance (h)
0.0
 
2.1
150
Combat
Guns (qt)
1
 
3
18
2 × fixed, forward-firing 7.92 mm (.312 in) machine guns; 1 × flexible 7.92 (.312 in) mm machine gun for observer
Bombs (qt)
1
 
2
250
50 kg bombs
Stat
Number built (qt)
0
 
4
43,000
Introduction 1928
First flight 1928

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