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    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      50 m2
      76 m2
    • Wingspan (Beam)
      19 m
      29 m
    • Wing loading
      88 kg/m2
      133 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
      3920 kg
      5880 kg
    • Max. takeoff weight (Gross weight)
      6000 kg
      9000 kg
    • Loaded weight
      5600 kg
      8400 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
      253 km/h
      381 km/h
    • Сruise Speed
      176 km/h
      264 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
      1136 hp
      1704 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5424 m
      8136 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1720 km
      2580 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
      216 m/min
      324 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
      2 qt
    • Bombs
      1 qt
      3 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
      24 qt
      38 qt
    • Price
      41 USD
      750000000 USD

Aichi H9A

TypeFlying boat
Company

Aichi Kokuki KK

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
17.0
88.7
Height (m)
0.6
 
5.3
50.1
Wings
Wing area (m2)
1.1
 
63.3
925
Wingspan (Beam) (m)
0.1
 
24
95
Wing loading (kg/m2)
3.1
 
110.6
829
Weights
Empty weight (kg)
8
 
4,900
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,500
575,000
Loaded weight (kg)
5
 
7,000
242,500
Capacity
Crew (per.)
1
 
5
112
Normal crew of 5 (and up to 3 pupils)
Speeds
Max. Speed (km/h)
25
 
317
28,165
at 3000 m
Сruise Speed (km/h)
52
 
220
3,087
at 1000 m
Power
Total Power (hp)
0.4
 
1,420
60,000
2 powerplants 710 hp each
Performance
Service ceiling (m)
0.6
 
6,780
161,544
Range (Ferry range) (km)
4
 
2,150
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
270
36,000
Combat
Guns (qt)
1
 
1
18
flexible, 7.7 mm (.303 in) Type 92 machine gun in bow and dorsal hatches
Bombs (qt)
1
 
2
250
250 kg bombs or depth-charges
Stat
Number built (qt)
0
 
31
43,000
Introduction 1940
First flight 01.09.1940
Stop production 1945

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