Search filter

    • Year
      1906
      2018
    • Length
      10 m
      17 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      40 m2
      62 m2
    • Wingspan (Beam)
      16 m
      24 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
      4320 kg
      6480 kg
    • Max. takeoff weight (Gross weight)
      6713 kg
      10070 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      8 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
      317 km/h
      477 km/h
    • Сruise Speed
      262 km/h
      394 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
      1760 hp
      2640 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5976 m
      8964 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2520 km
      3780 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
      297 m/min
      447 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      272 kg
      408 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      2352 qt
      3530 qt
    • Price
      41 USD
      750000000 USD

Lockheed A-28 Hudson

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
13.5
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
51.2
925
Wingspan (Beam) (m)
0.1
 
20
95
Weights
Empty weight (kg)
8
 
5,400
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,391.5
575,000
Capacity
Crew (per.)
1
 
6
112
Speeds
Max. Speed (km/h)
25
 
397
28,165
Сruise Speed (km/h)
52
 
328
3,087
Power
Total Power (hp)
0.4
 
2,200
60,000
2 powerplants 1100 hp each
Performance
Service ceiling (m)
0.6
 
7,470
161,544
Range (Ferry range) (km)
4
 
3,150
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
372
36,000
Combat
Guns (qt)
1
 
4
18
2 × .303 in (7.7 mm) Browning machine guns in dorsal turret; 2× .303 Browning machine guns in nose
Bombs weight (kg)
2
 
340
39,000
of bombs or depth charges
Stat
Number built (qt)
0
 
2,941
43,000
Introduction 1938
First flight 10.12.1938
Stop production 1943

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