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    • Year
      1906
      2018
    • Length
      32 m
      49 m
    • Height
      11 m
      18 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      130 m2
      197 m2
    • Wingspan (Beam)
      31 m
      48 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
      42637 kg
      63957 kg
    • Max. takeoff weight (Gross weight)
      91081 kg
      136623 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      25120 kg
      37680 kg
    • Capacity passengers
      120 per.
      180 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      519 km/h
      779 km/h
    • Max. Speed
      648 km/h
      974 km/h
    • Сruise Speed
      578 km/h
      868 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
      0 hp
      60000 hp
    • Thrust
      363 kN
      545 kN
    • Service ceiling
      10972 m
      16460 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4108 km
      6164 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
      1548 m/min
      2323 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Boeing YC-14

TypeAircraft
Company

Boeing

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
40.1
88.7
Height (m)
0.6
 
14.7
50.1
Wings
Wing area (m2)
1.1
 
163.7
925
Wingspan (Beam) (m)
0.1
 
39.3
95
Weights
Empty weight (kg)
8
 
53,297.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
113,851.7
575,000
conventional landing and takeoff
Capacity
Crew (per.)
1
 
3
112
Payload (kg)
23
 
31,400
122,470
Capacity passengers (per.)
1
 
150
400
troops
Speeds
Ground Speed (km/h)
96.6
 
649
1,500
Max. Speed (km/h)
25
 
811
28,165
Сruise Speed (km/h)
52
 
723
3,087
Power
Thrust (kN)
1.5
 
454
1,914
2 powerplants 227 kN each
Performance
Service ceiling (m)
0.6
 
13,716
161,544
Range (Ferry range) (km)
4
 
5,136
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,935.5
36,000
Stat
Number built (qt)
0
 
2
43,000
Introduction 1976
First flight 09.08.1976

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