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    • Year
      1906
      2018
    • Length
      26 m
      41 m
    • Height
      9 m
      14 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      36 m
      55 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
      27527 kg
      41292 kg
    • Max. takeoff weight (Gross weight)
      45359 kg
      68039 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
      338 km/h
      508 km/h
    • Сruise Speed
      236 km/h
      354 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
      8000 hp
      12000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4145 m
      6218 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5152 km
      7728 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      20 h
      31 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
      219 m/min
      330 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
      1 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
      1440 kg
      2160 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Shorts S.35 Shetland

TypeAircraft
Company

Short Brothers

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
33.5
88.7
Height (m)
0.6
 
11.3
50.1
Wings
Wingspan (Beam) (m)
0.1
 
45.8
95
Weights
Empty weight (kg)
8
 
34,409.5
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
56,699.1
575,000
Capacity
Crew (per.)
1
 
11
112
Speeds
Max. Speed (km/h)
25
 
423
28,165
Сruise Speed (km/h)
52
 
295
3,087
Power
Total Power (hp)
0.4
 
10,000
60,000
4 powerplant 2500 hp each
Performance
Service ceiling (m)
0.6
 
5,181.6
161,544
Range (Ferry range) (km)
4
 
6,440
40,700
Endurance (h)
0.0
 
25.8
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
274.3
36,000
Combat
Bombs weight (kg)
2
 
1,800
39,000
bombs or depth charges
Stat
Number built (qt)
0
 
2
43,000
Introduction 1944
First flight 14.12.1944

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