Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      90 m2
      136 m2
    • Wingspan (Beam)
      22 m
      34 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
      2887 kg
      4331 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      4440 kg
      6660 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
      109 km/h
      165 km/h
    • Сruise Speed
      52 km/h
      3087 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
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2633 m
      3951 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
      4 h
      8 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
      81 m/min
      123 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
      3 qt
      5 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
      382 qt
      574 qt
    • Price
      26527 USD
      39791 USD

Curtiss Model H

TypeFlying boat
Company

Curtiss Aeroplane and Motor Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
14.2
88.7
Height (m)
0.6
 
5.0
50.1
Wings
Wing area (m2)
1.1
 
113
925
Wingspan (Beam) (m)
0.1
 
28.3
95
Weights
Empty weight (kg)
8
 
3,609
276,800
Loaded weight (kg)
5
 
5,550
242,500
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
137
28,165
Performance
Service ceiling (m)
0.6
 
3,292
161,544
Endurance (h)
0.0
 
6
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
102
36,000
Combat
Guns (qt)
1
 
4
18
.303 in (7.7 mm) Lewis guns on flexible mounts
Bombs (qt)
1
 
2
250
105 kg bombs below the wings
1
 
4
250
45 kg bombs or
Stat
Number built (qt)
0
 
478
43,000
Price (USD)
41.5
 
33,159
750.0 million
Introduction 1917
First flight 23.06.1914
Stop production 1918

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