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    • Year
      1906
      2018
    • Length
      24 m
      38 m
    • Height
      9 m
      14 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      32 m
      50 m
    • Wing loading
      132 kg/m2
      200 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
      13682 kg
      20524 kg
    • Max. takeoff weight (Gross weight)
      26671 kg
      40007 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      5 per.
      9 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      30 per.
      46 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      268 km/h
      404 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
      4416 hp
      6624 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4121 km
      6183 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
      3 qt
      5 qt
    • Prop diameter
      3 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      51 qt
      77 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
      2 qt
      4 qt
    • Price
      41 USD
      750000000 USD

Shorts S.26 G-class

TypeFlying boat
Company

Short Brothers

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
30.9
88.7
Height (m)
0.6
 
11.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
40.9
95
Wing loading (kg/m2)
3.1
 
166
829
Weights
Empty weight (kg)
8
 
17,102.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
33,339.0
575,000
Capacity
Crew (per.)
1
 
7
112
Capacity passengers (per.)
1
 
38
400
Speeds
Max. Speed (km/h)
25
 
336
28,165
Power
Total Power (hp)
0.4
 
5,520
60,000
4 powerplants 1380 hp each
Performance
Range (Ferry range) (km)
4
 
5,152
40,700
Propellers
Propellers (qt)
1
 
4
8
1 per powerplant
Prop diameter (m)
1.8
 
4.4
5.8
Combat
Guns (qt)
1
 
3
18
2 × dorsal and 1 × tail Boulton Paul BPA Mk. II
Bombs (qt)
1
 
64
250
8 × 500 lb (227 kg) bombs under the wings; 20 × reconnaissance flares; 28 × flame floats; 8 × smoke floats
Stat
Number built (qt)
0
 
3
43,000
Introduction 1939
First flight 21.07.1939

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