Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      37 m2
      57 m2
    • Wingspan (Beam)
      14 m
      21 m
    • Wing loading
      173 kg/m2
      261 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
      5856 kg
      8784 kg
    • Max. takeoff weight (Gross weight)
      9208 kg
      13812 kg
    • Loaded weight
      8144 kg
      12216 kg
    • Crew
      1 per.
      3 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
      464 km/h
      696 km/h
    • Сruise Speed
      352 km/h
      528 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
      3200 hp
      4800 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1360 km
      2040 km
    • Range PTB (Ferry range)
      2000 km
      3000 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
      488 m/min
      732 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      3 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      3 qt
      5 qt
    • Guns
      4 qt
      8 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

Aichi S1A

TypeAircraft
Company

Aichi Kokuki KK

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
15.1
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
47
925
Wingspan (Beam) (m)
0.1
 
17.5
95
Wing loading (kg/m2)
3.1
 
217
829
Weights
Empty weight (kg)
8
 
7,320
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
11,510
575,000
Loaded weight (kg)
5
 
10,180
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
580
28,165
Сruise Speed (km/h)
52
 
440
3,087
Power
Total Power (hp)
0.4
 
4,000
60,000
2 powerplants 2000 hp each
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Range (Ferry range) (km)
4
 
1,700
40,700
Range PTB (Ferry range) (km)
720
 
2,500
10,000
Dynamic Performance
Rate of climb (m/min)
1.9
 
610
36,000
Propellers
Propellers (qt)
1
 
2
8
Prop blade number (qt)
1
 
4
8
Combat
Guns (qt)
1
 
6
18
2× fuselage-mounted forward-firing 30mm Type 5 cannon; 2× fuselage-mounted forward-firing 20mm Type 99 model 1 cannon; 2× dorsal turret-mounted 20mm Type 99 model 2 cannon
Stat
Introduction 1945

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