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    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      5 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 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
      217 m2
      326 m2
    • Main rotor diameter
      14 m
      23 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
      3 m
      5 m
    • Empty weight
      8400 kg
      12600 kg
    • Max. takeoff weight (Gross weight)
      11680 kg
      17520 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      247 km/h
      371 km/h
    • Сruise Speed
      222 km/h
      334 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
      3438 l
      5157 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
      5040 hp
      7560 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3660 m
      5490 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      666 km
      1000 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      4 h
      6 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
      3 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      16800000 USD
      25200000 USD

Boeing 101

TypeHelicopter
Company

Boeing

Geometry
Length (m)
1.9
 
19.5
88.7
Height (m)
0.6
 
6.6
50.1
Rotors
Disc area (m2)
1.4
 
271.5
460
Main rotor diameter (m)
1.2
 
18.6
62
Tail rotor diameter (m)
0.8
 
4
4.9
Weights
Empty weight (kg)
8
 
10,500
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,600
575,000
Capacity
Crew (per.)
1
 
4
112
3-4
Speeds
Max. Speed (km/h)
25
 
309
28,165
Сruise Speed (km/h)
52
 
278
3,087
Fuel
Fuel Capacity (l)
23
 
4,297.5
320,000
Power
Total Power (hp)
0.4
 
6,300
60,000
3 powerplants 2100 hp each
Performance
Service ceiling (m)
0.6
 
4,575
161,544
Range (Ferry range) (km)
4
 
833
40,700
Endurance (h)
0.0
 
5
150
Combat
Torpedoes (qt)
1
 
4
4
Sting Ray homing torpedoes or depth charges
Stat
Price (USD)
41.5
 
21.0 million
750.0 million
Introduction 1987
First flight 09.10.1987

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