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    • Year
      1906
      2018
    • Length
      9 m
      14 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      71 m2
      108 m2
    • Wingspan (Beam)
      14 m
      22 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
      1334 kg
      2002 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2236 kg
      3354 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
      96 km/h
      146 km/h
    • Сruise Speed
      86 km/h
      130 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
      160 hp
      240 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2598 m
      3898 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
      14 h
      22 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
      40 m/min
      62 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      48 min
      72 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Supermarine Nighthawk

TypeAircraft
Company

Supermarine Aviation Works

Scheme

Multiplane

Geometry
Length (m)
1.9
 
11.3
88.7
Height (m)
0.6
 
5.4
50.1
Wings
Wing area (m2)
1.1
 
89.4
925
Wingspan (Beam) (m)
0.1
 
18.3
95
Weights
Empty weight (kg)
8
 
1,667.9
276,800
Loaded weight (kg)
5
 
2,795
242,500
Capacity
Crew (per.)
1
 
4
112
2 pilots, 2 gunners
Speeds
Max. Speed (km/h)
25
 
121
28,165
Сruise Speed (km/h)
52
 
108
3,087
Power
Total Power (hp)
0.4
 
200
60,000
2 powerplants 100 hp each
Performance
Service ceiling (m)
0.6
 
3,248
161,544
Endurance (h)
0.0
 
18
150
theoretical
Dynamic Performance
Rate of climb (m/min)
1.9
 
51
36,000
Time to altitude (min)
0.6
 
60
105
to 3050 m
Combat
Guns (qt)
1
 
3
18
One 1½-pdr Davis gun and one Lewis gun above upper wing, and one Lewis gun in the nose
Stat
Number built (qt)
0
 
1
43,000
Introduction 1916
First flight 1917

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