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    • Year
      1906
      2018
    • Length
      21 m
      32 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      125 m2
      189 m2
    • Wingspan (Beam)
      27 m
      42 m
    • Wing loading
      139 kg/m2
      209 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
      14332 kg
      21500 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      21818 kg
      32728 kg
    • Crew
      4 per.
      6 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
      265 km/h
      399 km/h
    • Сruise Speed
      226 km/h
      340 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
      3840 hp
      5760 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4364 m
      6548 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3142 km
      4714 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
      204 m/min
      308 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Shorts S.25 Sandringham

TypeAircraft
Company

Short Brothers

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
26.3
88.7
Height (m)
0.6
 
7.0
50.1
Wings
Wing area (m2)
1.1
 
156.7
925
Wingspan (Beam) (m)
0.1
 
34.4
95
Wing loading (kg/m2)
3.1
 
174
829
Weights
Empty weight (kg)
8
 
17,916.0
276,800
Loaded weight (kg)
5
 
27,273
242,500
Capacity
Crew (per.)
1
 
5
112
Speeds
Max. Speed (km/h)
25
 
332
28,165
Сruise Speed (km/h)
52
 
283
3,087
Power
Total Power (hp)
0.4
 
4,800
60,000
4 powerplants 1200 hp each
Performance
Service ceiling (m)
0.6
 
5,455.9
161,544
Range (Ferry range) (km)
4
 
3,928
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
256.0
36,000
Stat
Introduction 1945
First flight 16.10.1937
Stop production 1974

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