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    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      7 m
      11 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
      6489 kg
      9735 kg
    • Max. takeoff weight (Gross weight)
      12720 kg
      19080 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
      2176 km/h
      3264 km/h
    • Сruise Speed
      52 km/h
      3087 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
      88 kN/kg
      134 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      53 kN
      81 kN
    • Service ceiling
      14640 m
      21960 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2720 km
      4080 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      352 m
      528 m
    • Landing roll
      744 m
      1116 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      14400 m/min
      21600 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Lockheed X-27 Lancer

TypeAircraft
Company

Lockheed Corporation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
17.5
88.7
Height (m)
0.6
 
5.2
50.1
Wings
Wingspan (Beam) (m)
0.1
 
8.9
95
Weights
Empty weight (kg)
8
 
8,112
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
15,900
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
2,720
28,165
Power
Afterburning thrust (kN/kg)
29.4
 
111.2
980
1 powerplant
Thrust (kN)
1.5
 
66.7
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
18,300
161,544
more than 18300
Range (Ferry range) (km)
4
 
3,400
40,700
with 8800 kg
Takeoff roll (m)
20
 
440
3,200
Landing roll (m)
20
 
930
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
18,000
36,000
Stat
Introduction 1968

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