Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      9 m
      15 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
      6549 kg
      9825 kg
    • Max. takeoff weight (Gross weight)
      11350 kg
      17026 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
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      851 km/h
      1277 km/h
    • Сruise Speed
      608 km/h
      914 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      29 kN
      44 kN
    • Service ceiling
      9509 m
      14265 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2944 km
      4416 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
      1353 m/min
      2031 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
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      6 qt
      10 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      725 kg
      1089 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      4080000 USD
      6120000 USD

Lockheed F-90

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
17.1
88.7
Height (m)
0.6
 
4.8
50.1
Wings
Wing area (m2)
1.1
 
32.1
925
Wingspan (Beam) (m)
0.1
 
12.2
95
Weights
Empty weight (kg)
8
 
8,187.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,188
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,064
28,165
Сruise Speed (km/h)
52
 
761
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Thrust (kN)
1.5
 
36.4
1,914
2 powerplants 18,2 kN each
Performance
Service ceiling (m)
0.6
 
11,887.2
161,544
Range (Ferry range) (km)
4
 
3,680
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,692
36,000
Combat
Guns (qt)
1
 
6
18
20 mm (.79 in) cannons
Rockets (qt)
1
 
8
76
5 in (127 mm) HVAR rockets
Bombs weight (kg)
2
 
907
39,000
of bombs
Stat
Number built (qt)
0
 
2
43,000
Price (USD)
41.5
 
5.1 million
750.0 million
Introduction 1949
First flight 03.06.1949

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