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    • Year
      1906
      2018
    • Length
      14 m
      23 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      40 m2
      61 m2
    • Wingspan (Beam)
      13 m
      20 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
      8981 kg
      13472 kg
    • Max. takeoff weight (Gross weight)
      16147 kg
      24222 kg
    • Loaded weight
      15072 kg
      22608 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      8 per.
      12 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      706 km/h
      1060 km/h
    • Сruise Speed
      648 km/h
      974 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
      8056 l
      12084 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
      0 hp
      60000 hp
    • Thrust
      52 kN
      80 kN
    • Service ceiling
      10485 m
      15728 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3856 km
      5784 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
      1011 m/min
      1518 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
      163 qt
      245 qt
    • Price
      41 USD
      750000000 USD

Lockheed JetStar

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
18.4
88.7
Height (m)
0.6
 
6.2
50.1
Wings
Wing area (m2)
1.1
 
50.4
925
Wingspan (Beam) (m)
0.1
 
16.6
95
Weights
Empty weight (kg)
8
 
11,226.4
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
20,184.9
575,000
Loaded weight (kg)
5
 
18,840
242,500
Capacity
Crew (per.)
1
 
3
112
2 pilots & typically 1 flight attendant
Capacity passengers (per.)
1
 
10
400
8-10 passengers
Speeds
Max. Speed (km/h)
25
 
883
28,165
at 9145 m
Сruise Speed (km/h)
52
 
811
3,087
Fuel
Fuel Capacity (l)
23
 
10,070
320,000
Power
Thrust (kN)
1.5
 
66
1,914
4 powerplants 16,5 kN each
Performance
Service ceiling (m)
0.6
 
13,106.4
161,544
Range (Ferry range) (km)
4
 
4,820
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,264.9
36,000
Stat
Number built (qt)
0
 
204
43,000
Introduction 1957
First flight 04.09.1957
Stop production 1990

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