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
      100 m2
      152 m2
    • Wingspan (Beam)
      20 m
      30 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
      2360 kg
      3540 kg
    • Max. takeoff weight (Gross weight)
      3920 kg
      5880 kg
    • Loaded weight
      3920 kg
      5880 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      6 per.
      10 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      144 km/h
      216 km/h
    • Сruise Speed
      124 km/h
      186 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
      576 hp
      864 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4800 m
      7200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      480 km
      720 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
      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
      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
      4 qt
      8 qt
    • Price
      41 USD
      750000000 USD

Blériot 115

TypeAircraft
Company

Blériot Aéronautique

Scheme

Biplane

Geometry
Length (m)
1.9
 
14.5
88.7
Height (m)
0.6
 
5.0
50.1
Wings
Wing area (m2)
1.1
 
126
925
Wingspan (Beam) (m)
0.1
 
25
95
Weights
Empty weight (kg)
8
 
2,950
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,900
575,000
Loaded weight (kg)
5
 
4,900
242,500
Capacity
Crew (per.)
1
 
3
112
Two pilots and one radio operator
Capacity passengers (per.)
1
 
8
400
Speeds
Max. Speed (km/h)
25
 
180
28,165
Сruise Speed (km/h)
52
 
155
3,087
Power
Total Power (hp)
0.4
 
720
60,000
4 powerplants 180 hp each
Performance
Service ceiling (m)
0.6
 
6,000
161,544
Range (Ferry range) (km)
4
 
600
40,700
Stat
Number built (qt)
0
 
6
43,000
Introduction 1923
First flight 09.05.1923

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