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    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      23 m2
      35 m2
    • Wingspan (Beam)
      11 m
      18 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
      2576 kg
      3864 kg
    • Max. takeoff weight (Gross weight)
      3760 kg
      5640 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
      344 km/h
      516 km/h
    • Max. Speed
      388 km/h
      582 km/h
    • Сruise Speed
      367 km/h
      551 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
      1120 hp
      1680 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6720 m
      10080 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      880 km
      1320 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
      408 m/min
      613 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
      4 qt
      8 qt
    • Bombs
      8 qt
      12 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
      728 qt
      1092 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-51

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
10.5
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
29
925
Wingspan (Beam) (m)
0.1
 
14.3
95
Weights
Empty weight (kg)
8
 
3,220
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,700
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
430
1,500
Max. Speed (km/h)
25
 
485
28,165
Сruise Speed (km/h)
52
 
459
3,087
Power
Total Power (hp)
0.4
 
1,400
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,400
161,544
Range (Ferry range) (km)
4
 
1,100
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
510.2
36,000
Combat
Guns (qt)
1
 
6
18
4 in the wings, 1 in upper turret, 1 in the hatch in the floor
Bombs (qt)
1
 
10
250
10 × RS-82 rockets or 8 × RS-132 rockets
Stat
Number built (qt)
0
 
910
43,000
Introduction 1937
First flight 25.08.1937

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