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    • Year
      1906
      2018
    • Length
      28 m
      43 m
    • Height
      9 m
      15 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      96 m2
      145 m2
    • Wingspan (Beam)
      24 m
      37 m
    • Wing loading
      424 kg/m2
      636 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
      28013 kg
      42021 kg
    • Max. takeoff weight (Gross weight)
      51528 kg
      77293 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      8 per.
      14 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      14 qt
      22 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      600 km/h
      900 km/h
    • Сruise Speed
      488 km/h
      732 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
      28350 l
      42525 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
      15872 hp
      23808 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6900 m
      10352 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3526 km
      5290 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1992 km
      2988 km
    • Endurance
      12 h
      20 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
      3 qt
      5 qt
    • Prop diameter
      3 m
      5 m
    • Prop blade number
      3 qt
      5 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
      520 qt
      780 qt
    • Price
      28800000 USD
      43200000 USD

Lockheed P-3 Orion

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
35.6
88.7
Height (m)
0.6
 
11.8
50.1
Wings
Wing area (m2)
1.1
 
120.8
925
Wingspan (Beam) (m)
0.1
 
30.4
95
Wing loading (kg/m2)
3.1
 
530
829
Weights
Empty weight (kg)
8
 
35,017.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
64,410.1
575,000
Capacity
Crew (per.)
1
 
11
112
Hardpoints (qt)
1
 
18
2,576
10 wing stations in total and 8 internal bomb bay stations with a capacity of 9,100 kg
Speeds
Max. Speed (km/h)
25
 
750
28,165
Сruise Speed (km/h)
52
 
610
3,087
Fuel
Fuel Capacity (l)
23
 
35,437.5
320,000
Power
Total Power (hp)
0.4
 
19,840
60,000
4 powerplants 4960 hp each
Performance
Service ceiling (m)
0.6
 
8,625.8
161,544
Range (Ferry range) (km)
4
 
4,407.8
40,700
Сombat radius (km)
277
 
2,490
7,210
three hours on-station at 457 m
Endurance (h)
0.0
 
16
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
960
36,000
Propellers
Propellers (qt)
1
 
4
8
1 per engine
Prop diameter (m)
1.8
 
4.1
5.8
Prop blade number (qt)
1
 
4
8
Stat
Number built (qt)
0
 
650
43,000
Price (USD)
41.5
 
36.0 million
750.0 million
Introduction 1958
First flight 01.11.1959

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