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    • Year
      1906
      2018
    • Length
      20 m
      32 m
    • Height
      8 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      110 m2
      167 m2
    • Wingspan (Beam)
      27 m
      42 m
    • Wing loading
      152 kg/m2
      230 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
      12519 kg
      18779 kg
    • Max. takeoff weight (Gross weight)
      21852 kg
      32780 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      8 per.
      14 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
      268 km/h
      404 km/h
    • Сruise Speed
      228 km/h
      342 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
      3408 hp
      5112 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3901 m
      5853 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2278 km
      3418 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
      176 m/min
      265 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
      14 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
      621 qt
      933 qt
    • Price
      41 USD
      750000000 USD

Shorts S.25 Sunderland

TypeAircraft
Company

Short Brothers

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
26
88.7
Height (m)
0.6
 
10
50.1
Wings
Wing area (m2)
1.1
 
138.4
925
Wingspan (Beam) (m)
0.1
 
34.4
95
Wing loading (kg/m2)
3.1
 
191
829
Weights
Empty weight (kg)
8
 
15,648.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
27,316
575,000
Capacity
Crew (per.)
1
 
11
112
two pilots, radio operator, navigator, engineer, bomb-aimer, three to five gunners
Speeds
Max. Speed (km/h)
25
 
336
28,165
at 2000 m
Сruise Speed (km/h)
52
 
285
3,087
at 1500 m
Power
Total Power (hp)
0.4
 
4,260
60,000
4 powerplants 1065 hp each
Performance
Service ceiling (m)
0.6
 
4,876.8
161,544
Range (Ferry range) (km)
4
 
2,848
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
220.2
36,000
Combat
Guns (qt)
1
 
18
18
16× 0.303 inch (7.7 mm) Browning machine guns; 2× Browning 0.5 inch (12.7 mm) machine gun
Stat
Number built (qt)
0
 
777
43,000
Introduction 1937
First flight 16.10.1937
Stop production 1959

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