Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      27 m2
      41 m2
    • Wingspan (Beam)
      9 m
      15 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
      1029 kg
      1545 kg
    • Max. takeoff weight (Gross weight)
      1448 kg
      2172 kg
    • Loaded weight
      1431 kg
      2147 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
      208 km/h
      312 km/h
    • Max. Speed
      165 km/h
      249 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
      400 hp
      600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6400 m
      9600 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
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      13 min
      21 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      3 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Hanriot H.31

TypeAircraft
Company

Aéroplanes Hanriot et Cie

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.6
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
34
925
Wingspan (Beam) (m)
0.1
 
12
95
Weights
Empty weight (kg)
8
 
1,287
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,810
575,000
Loaded weight (kg)
5
 
1,789
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
260
1,500
Max. Speed (km/h)
25
 
207
28,165
at 5000 m
Сruise Speed (km/h)
52
 
220
3,087
Power
Total Power (hp)
0.4
 
500
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,000
161,544
Dynamic Performance
Time to altitude (min)
0.6
 
16.7
105
to 5000 m
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
2
8
Combat
Guns (qt)
1
 
4
18
7.7 mm (0.303 in) synchronised machine guns
Stat
Number built (qt)
0
 
1
43,000
Introduction 1925
First flight 1925

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