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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      24 m2
      36 m2
    • Wingspan (Beam)
      7 m
      12 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
      693 kg
      1041 kg
    • Max. takeoff weight (Gross weight)
      1044 kg
      1568 kg
    • Loaded weight
      1044 kg
      1568 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
      173 km/h
      261 km/h
    • Сruise Speed
      173 km/h
      261 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
      240 hp
      360 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6400 m
      9600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      320 km
      480 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
      268 m/min
      404 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
      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
      80 qt
      120 qt
    • Price
      41 USD
      750000000 USD

Blériot Blériot-SPAD S.XX

TypeAircraft
Company

Blériot Aéronautique

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.3
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
30
925
Wingspan (Beam) (m)
0.1
 
9.7
95
Weights
Empty weight (kg)
8
 
867
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,306
575,000
Loaded weight (kg)
5
 
1,306
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and gunner
Speeds
Max. Speed (km/h)
25
 
217
28,165
Сruise Speed (km/h)
52
 
217
3,087
Power
Total Power (hp)
0.4
 
300
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,000
161,544
Range (Ferry range) (km)
4
 
400
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
336
36,000
Combat
Guns (qt)
1
 
3
18
2 × fixed, forward-firing .303 Vickers machine guns; 1 × trainable, rearward-firing .303 Lewis gun
Stat
Number built (qt)
0
 
100
43,000
ca. 100
Introduction 1918
First flight 1918

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