Search filter

    • Year
      1906
      2018
    • Length
      39 m
      60 m
    • Height
      11 m
      18 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      56 m
      85 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
      60296 kg
      90446 kg
    • Max. takeoff weight (Gross weight)
      148778 kg
      223168 kg
    • Loaded weight
      95454 kg
      143182 kg
    • Crew
      10 per.
      16 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
      537 km/h
      807 km/h
    • Сruise Speed
      296 km/h
      444 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
      18240 hp
      27360 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      10631 m
      15948 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      5132 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
      486 m/min
      730 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      4 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      2 qt
      4 qt
    • Guns
      1 qt
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      26160 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      307 qt
      461 qt
    • Price
      3280000 USD
      4920000 USD

Convair Model 36 B-36 Peacemaker

TypeAircraft
Company

Consolidated Vultee Convair

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
49.4
88.7
Height (m)
0.6
 
14.3
50.1
Wings
Wingspan (Beam) (m)
0.1
 
70.1
95
Weights
Empty weight (kg)
8
 
75,371.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
185,972.9
575,000
Loaded weight (kg)
5
 
119,318
242,500
combat weight
Capacity
Crew (per.)
1
 
13
112
Speeds
Max. Speed (km/h)
25
 
672
28,165
Сruise Speed (km/h)
52
 
370
3,087
Power
Total Power (hp)
0.4
 
22,800
60,000
6 powerplants 3800 hp each
Performance
Service ceiling (m)
0.6
 
13,289.3
161,544
Сombat radius (km)
277
 
6,415
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
608.1
36,000
Propellers
Propellers (qt)
1
 
6
8
1 per engine
Prop blade number (qt)
1
 
3
8
per propeller
Combat
Guns (qt)
1
 
2
18
1
 
2
18
20 mm (0.787 in) M24A1 autocannons
Bombs weight (kg)
2
 
39,000
39,000
with weight restrictions
2
 
32,700
39,000
normal
Stat
Number built (qt)
0
 
384
43,000
Price (USD)
41.5
 
4.1 million
750.0 million
Introduction 1946
First flight 08.08.1946
Stop production 12.02.1959

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