Search filter

    • Year
      1906
      2018
    • Length
      26 m
      40 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      136 m2
      204 m2
    • Wingspan (Beam)
      13 m
      21 m
    • Wing loading
      328 kg/m2
      492 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      3
    • 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
      24480 kg
      36720 kg
    • Max. takeoff weight (Gross weight)
      62414 kg
      93622 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      1270 kg
      1906 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      2832 km/h
      4248 km/h
    • Сruise Speed
      2469 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
      36944 l
      55416 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
      241 kN/kg
      363 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      20726 m
      31090 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4320 km
      6480 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
      2882 m/min
      4324 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
      25 qt
      39 qt
    • Price
      41 USD
      750000000 USD

Lockheed SR-71 Blackbird

TypeAircraft
Company

Lockheed Corporation

Scheme

Integrated

Monoplane

Geometry
Length (m)
1.9
 
32.7
88.7
Height (m)
0.6
 
5.6
50.1
Wings
Wing area (m2)
1.1
 
170
925
Wingspan (Beam) (m)
0.1
 
16.9
95
Wing loading (kg/m2)
3.1
 
410
829
Aspect ratio
1.7
 
1.7
25.6
Weights
Empty weight (kg)
8
 
30,600
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
78,017.9
575,000
Capacity
Crew (per.)
1
 
2
112
Pilot and Reconnaissance Systems Officer
Payload (kg)
23
 
1,587.6
122,470
of sensors
Speeds
Max. Speed (km/h)
25
 
3,540
28,165
at 24000
Сruise Speed (km/h)
52
 
3,087
3,087
Fuel
Fuel Capacity (l)
23
 
46,180
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Afterburning thrust (kN/kg)
29.4
 
302
980
151 kN each
Performance
Service ceiling (m)
0.6
 
25,908
161,544
Range (Ferry range) (km)
4
 
5,400
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
3,602.7
36,000
Stat
Number built (qt)
0
 
32
43,000
Introduction 1964
First flight 22.12.1964
Stop production 1998

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