Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      28 m2
      44 m2
    • Wingspan (Beam)
      5 m
      9 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
      3247 kg
      4872 kg
    • Max. takeoff weight (Gross weight)
      4535 kg
      6804 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
      772 km/h
      1160 km/h
    • Сruise Speed
      364 km/h
      548 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
      1270 l
      1906 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
      10 kN
      16 kN
    • Service ceiling
      8160 m
      12240 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      2 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
      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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Lockheed Have Blue

TypeAircraft
Company

Lockheed Corporation

Scheme

Integrated

Monoplane

Geometry
Length (m)
1.9
 
14.4
88.7
Height (m)
0.6
 
2.3
50.1
Wings
Wing area (m2)
1.1
 
35.9
925
Wingspan (Beam) (m)
0.1
 
6.9
95
Weights
Empty weight (kg)
8
 
4,059.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,669.9
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
966
28,165
Сruise Speed (km/h)
52
 
456
3,087
Fuel
Fuel Capacity (l)
23
 
1,588
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.5
2.1
0.46–0.62
Thrust (kN)
1.5
 
13.1
1,914
Performance
Service ceiling (m)
0.6
 
10,200
161,544
Endurance (h)
0.0
 
1
150
Stat
Number built (qt)
0
 
2
43,000
Introduction 1977
First flight 01.12.1977
Stop production 1979

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