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    • Year
      1906
      2018
    • Length
      25 m
      39 m
    • Height
      9 m
      15 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      337 m2
      507 m2
    • Wingspan (Beam)
      43 m
      65 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
      17120 kg
      25680 kg
    • Max. takeoff weight (Gross weight)
      29600 kg
      44400 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      9 per.
      15 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
      160 km/h
      240 km/h
    • Max. Speed
      150 km/h
      226 km/h
    • Сruise Speed
      52 km/h
      3087 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
      3600 hp
      5400 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2200 m
      3300 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      800 km
      1200 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      800 km
      1200 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      640 m
      960 m
    • Landing roll
      320 m
      480 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      64 m/min
      98 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      1 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      5 qt
      9 qt
    • Bombs
      32 qt
      48 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-16

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
32
88.7
Height (m)
0.6
 
11.7
50.1
Wings
Wing area (m2)
1.1
 
422
925
Wingspan (Beam) (m)
0.1
 
54
95
Weights
Empty weight (kg)
8
 
21,400
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
37,000
575,000
Capacity
Crew (per.)
1
 
12
112
Speeds
Ground Speed (km/h)
96.6
 
200
1,500
Max. Speed (km/h)
25
 
188
28,165
Power
Total Power (hp)
0.4
 
4,500
60,000
6 powerplants
Performance
Service ceiling (m)
0.6
 
2,750
161,544
Range (Ferry range) (km)
4
 
1,000
40,700
Сombat radius (km)
277
 
1,000
7,210
Takeoff roll (m)
20
 
800
3,200
Landing roll (m)
20
 
400
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
81
36,000
Time to altitude (min)
0.6
 
0.6
105
to 2000 m
Combat
Guns (qt)
1
 
7
18
2x20mm cannon, 5x2 7.62mm DA machine guns
Bombs (qt)
1
 
40
250
Stat
Number built (qt)
0
 
1
43,000
Introduction 1933
First flight 03.07.1933

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