Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      27 m2
      42 m2
    • Wingspan (Beam)
      12 m
      19 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
      1088 kg
      1632 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1760 kg
      2640 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      8 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      184 km/h
      276 km/h
    • Сruise Speed
      148 km/h
      224 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
      464 hp
      696 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5111 m
      7667 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      632 km
      948 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
      420 m/min
      632 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
      3 qt
      5 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
      500 qt
      750 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi 4MS1

TypeAircraft
Company

Mitsubishi Aircraft Corporation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
9.5
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
34.5
925
Wingspan (Beam) (m)
0.1
 
15.8
95
Weights
Empty weight (kg)
8
 
1,360
276,800
Loaded weight (kg)
5
 
2,200
242,500
Capacity
Crew (per.)
1
 
4
112
Capacity passengers (per.)
1
 
6
400
Speeds
Max. Speed (km/h)
25
 
230
28,165
Сruise Speed (km/h)
52
 
186
3,087
Power
Total Power (hp)
0.4
 
580
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,389
161,544
Range (Ferry range) (km)
4
 
790
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
526
36,000
Combat
Guns (qt)
1
 
1
18
7.7 mm Type 92 machine gun
Bombs (qt)
1
 
4
250
30 kg (66 lb) bombs
Stat
Number built (qt)
0
 
625
43,000
Introduction 1930
First flight 1930

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