Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      39 m2
      60 m2
    • Wingspan (Beam)
      14 m
      22 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
      3 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
      1726 kg
      2590 kg
    • Max. takeoff weight (Gross weight)
      2903 kg
      4355 kg
    • Loaded weight
      2902 kg
      4355 kg
    • Crew
      1 per.
      2 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
      203 km/h
      305 km/h
    • Сruise Speed
      173 km/h
      261 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
      460 hp
      690 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3584 m
      5377 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      740 km
      1110 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
      1 m/min
      36000 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
      3 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Boeing 200 Monomail

TypeAircraft
Company

Boeing

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
13
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
49.7
925
Wingspan (Beam) (m)
0.1
 
18
95
Rotors
Rotor number (qt)
1
 
2
8
Weights
Empty weight (kg)
8
 
2,158
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,629
575,000
Loaded weight (kg)
5
 
3,628.7
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
6
400
Speeds
Max. Speed (km/h)
25
 
254
28,165
Сruise Speed (km/h)
52
 
217
3,087
Power
Total Power (hp)
0.4
 
575
60,000
Performance
Service ceiling (m)
0.6
 
4,480.5
161,544
Range (Ferry range) (km)
4
 
925
40,700
Propellers
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
2
43,000
Introduction 1930
First flight 06.05.1930
Stop production 1933

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