Search filter

    • Year
      1906
      2018
    • Length
      16 m
      25 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      58 m2
      88 m2
    • Wingspan (Beam)
      10 m
      16 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      53 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
      10704 kg
      16056 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      3 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      794 km/h
      1192 km/h
    • Сruise Speed
      244 km/h
      368 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
      6604 l
      9906 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      76 kN
      116 kN
    • Service ceiling
      10972 m
      16460 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1376 km
      2064 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
      4 G
      8 G
    • Rate of climb
      1 m/min
      36000 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
      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
      51 qt
      77 qt
    • Price
      34080000 USD
      51120000 USD

Lockheed F-117A Nighthawk

TypeAircraft
Company

Lockheed Corporation

Scheme

Integrated

Monoplane

Geometry
Length (m)
1.9
 
20.1
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
73
925
Wingspan (Beam) (m)
0.1
 
13.2
95
Sweep (deg)
25
 
67.3
67.3
Weights
Empty weight (kg)
8
 
13,380
276,800
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
2
2,576
Speeds
Max. Speed (km/h)
25
 
993
28,165
Сruise Speed (km/h)
52
 
306
3,087
Fuel
Fuel Capacity (l)
23
 
8,255
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Thrust (kN)
1.5
 
96
1,914
2 powerplants 48 kN each
Performance
Service ceiling (m)
0.6
 
13,716
161,544
Range (Ferry range) (km)
4
 
1,720
40,700
Dynamic Performance
Load factor from (G)
2
 
6
9
Stat
Number built (qt)
0
 
64
43,000
Price (USD)
41.5
 
42.6 million
750.0 million
Introduction 1981
First flight 18.06.1981
Stop production 22.04.2008

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