Search filter

    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      5 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      110 m2
      166 m2
    • Wingspan (Beam)
      26 m
      40 m
    • Wing loading
      112 kg/m2
      168 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
      10886 kg
      16330 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      16329 kg
      24495 kg
    • Crew
      4 per.
      6 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      30 per.
      46 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      309 km/h
      465 km/h
    • Сruise Speed
      275 km/h
      413 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
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      3520 hp
      5280 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5688 m
      8532 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2256 km
      3384 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
      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
      8 qt
      12 qt
    • Price
      252000 USD
      378000 USD

Boeing 307 Stratoliner

TypeAircraft
Company

Boeing

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
22.6
88.7
Height (m)
0.6
 
6.3
50.1
Wings
Wing area (m2)
1.1
 
138
925
Wingspan (Beam) (m)
0.1
 
32.6
95
Wing loading (kg/m2)
3.1
 
140
829
Weights
Empty weight (kg)
8
 
13,608
276,800
Loaded weight (kg)
5
 
20,412
242,500
Capacity
Crew (per.)
1
 
5
112
two pilots, flight engineer, two cabin crew
Capacity passengers (per.)
1
 
38
400
38 passengers in daytime, 25 by night
Speeds
Max. Speed (km/h)
25
 
387
28,165
Сruise Speed (km/h)
52
 
344
3,087
Power
Power/mass (hp/kg)
0.0
 
0.2
22.1
Total Power (hp)
0.4
 
4,400
60,000
4 powerplants 1100 hp each
Performance
Service ceiling (m)
0.6
 
7,110
161,544
Range (Ferry range) (km)
4
 
2,820
40,700
Stat
Number built (qt)
0
 
10
43,000
Price (USD)
41.5
 
315,000
750.0 million
Introduction 1938
First flight 31.12.1938
Stop production 1975

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