Search filter

    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      22 m2
    • Wingspan (Beam)
      7 m
      11 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
      656 kg
      984 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      920 kg
      1380 kg
    • Crew
      1 per.
      2 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
      25 km/h
      28165 km/h
    • Сruise Speed
      176 km/h
      264 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
      208 hp
      312 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6800 m
      10200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      600 km
      900 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
      2 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      3 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Hanriot H.26

TypeAircraft
Company

Aéroplanes Hanriot et Cie

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.4
88.7
Height (m)
0.6
 
2.5
50.1
Wings
Wing area (m2)
1.1
 
18
925
Wingspan (Beam) (m)
0.1
 
9.1
95
Weights
Empty weight (kg)
8
 
820
276,800
Loaded weight (kg)
5
 
1,150
242,500
5
 
1,150
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Сruise Speed (km/h)
52
 
220
3,087
Power
Total Power (hp)
0.4
 
260
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,500
161,544
Range (Ferry range) (km)
4
 
750
40,700
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
1
43,000
Introduction 1923
First flight 1923

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