Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      95 m2
      143 m2
    • Wingspan (Beam)
      18 m
      28 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
      2335 kg
      3503 kg
    • Max. takeoff weight (Gross weight)
      4480 kg
      6720 kg
    • Loaded weight
      4480 kg
      6720 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      12 per.
      20 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      148 km/h
      222 km/h
    • Сruise Speed
      126 km/h
      190 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
      1344 hp
      2016 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      420 km
      630 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
      105 m/min
      159 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Blériot 165

TypeAircraft
Company

Blériot Aéronautique

Scheme

Biplane

Geometry
Length (m)
1.9
 
14.8
88.7
Height (m)
0.6
 
4.9
50.1
Wings
Wing area (m2)
1.1
 
119.1
925
Wingspan (Beam) (m)
0.1
 
23
95
Weights
Empty weight (kg)
8
 
2,919
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,600
575,000
Loaded weight (kg)
5
 
5,600
242,500
Capacity
Crew (per.)
1
 
3
112
Capacity passengers (per.)
1
 
16
400
Speeds
Max. Speed (km/h)
25
 
185
28,165
Сruise Speed (km/h)
52
 
158
3,087
Power
Total Power (hp)
0.4
 
1,680
60,000
4 powerplants 420 hp each
Performance
Service ceiling (m)
0.6
 
4,000
161,544
Range (Ferry range) (km)
4
 
525
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
132
36,000
Stat
Number built (qt)
0
 
2
43,000
Introduction 1926
First flight 27.10.1926

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