Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      70 m2
      106 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
      3000 kg
      4500 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      3972 kg
      5960 kg
    • Crew
      3 per.
      5 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
      159 km/h
      239 km/h
    • Сruise Speed
      134 km/h
      202 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
      880 hp
      1320 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5960 m
      8940 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
      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
      256 m/min
      386 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      800 kg
      1200 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      35 qt
      53 qt
    • Price
      41 USD
      750000000 USD

Blériot 127

TypeAircraft
Company

Blériot Aéronautique

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
14.7
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
88
925
Wingspan (Beam) (m)
0.1
 
23.2
95
Weights
Empty weight (kg)
8
 
3,750
276,800
Loaded weight (kg)
5
 
4,966
242,500
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
199
28,165
Сruise Speed (km/h)
52
 
168
3,087
Power
Total Power (hp)
0.4
 
1,100
60,000
2 powerplants
Performance
Service ceiling (m)
0.6
 
7,450
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
321
36,000
Combat
Guns (qt)
1
 
4
18
2 &times forward trainable Lewis guns in nose; 2 &times rearward trainable Lewis guns in each of two engine nacelles
Bombs weight (kg)
2
 
1,000
39,000
of bombs carried in internal bay
Stat
Number built (qt)
0
 
44
43,000
Introduction 1926
First flight 07.05.1926
Stop production 1934

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