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    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      12 m2
      19 m2
    • Wingspan (Beam)
      13 m
      21 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
      58 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      3658 kg
      5489 kg
    • Max. takeoff weight (Gross weight)
      4800 kg
      7200 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      445 km/h
      669 km/h
    • Сruise Speed
      296 km/h
      446 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
      2480 hp
      3720 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7072 m
      10608 m
    • Static ceiling
      2108 m
      3162 m
    • Range (Ferry range)
      659 km
      989 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
      768 m/min
      1152 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

Bell XV-15

TypeHelicopter
Company

Bell Aircraft Corporation

Scheme

Low wing

High wing

Geometry
Length (m)
1.9
 
12.8
88.7
Height (m)
0.6
 
3.9
50.1
Wings
Wing area (m2)
1.1
 
15.7
925
Wingspan (Beam) (m)
0.1
 
17.4
95
Rotors
Disc loading (kg/m2)
17.1
 
73
73
Weights
Empty weight (kg)
8
 
4,573.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,000
575,000
Capacity
Crew (per.)
1
 
2
112
pilot, copilot
Speeds
Max. Speed (km/h)
25
 
557
28,165
Сruise Speed (km/h)
52
 
371
3,087
Power
Total Power (hp)
0.4
 
3,100
60,000
2 powerplants 1550 hp each
Performance
Service ceiling (m)
0.6
 
8,840
161,544
Static ceiling (m)
3
 
2,635
5,485
Range (Ferry range) (km)
4
 
824.1
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
960
36,000
Stat
Number built (qt)
0
 
2
43,000
Introduction 1977
First flight 03.05.1977
Stop production 2003

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