Search filter

    • Year
      1906
      2018
    • Length
      9 m
      14 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 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
      3020 kg
      4530 kg
    • Max. takeoff weight (Gross weight)
      5492 kg
      8238 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      776 km/h
      1164 km/h
    • Сruise Speed
      576 km/h
      864 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
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      18 kN
      28 kN
    • Service ceiling
      11704 m
      17557 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1640 km
      2460 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      2 h
      4 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
      4 qt
      8 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
      5245 qt
      7869 qt
    • Price
      41 USD
      750000000 USD

Lockheed T-33 Shooting Star

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.5
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
21.8
925
Wingspan (Beam) (m)
0.1
 
11.9
95
Weights
Empty weight (kg)
8
 
3,775
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,865
575,000
Capacity
Crew (per.)
1
 
2
112
Hardpoints (qt)
1
 
2
2,576
with a capacity of907 kg of bombs or rocket pods each
Speeds
Max. Speed (km/h)
25
 
970
28,165
Сruise Speed (km/h)
52
 
720
3,087
Power
Thrust (kN)
1.5
 
23
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
14,630.4
161,544
Range (Ferry range) (km)
4
 
2,050
40,700
Endurance (h)
0.0
 
3.1
150
Combat
Guns (qt)
1
 
6
18
4 × 0.50 in (12.7 mm) Browning M3 machine guns with 650 rpg (for AT-33); 2 x 1.18 in (30mm) Oldsmobile M4 cannons with 350 rpg (AT-33)
Stat
Number built (qt)
0
 
6,557
43,000
Introduction 1948
First flight 22.03.1948

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