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    • Year
      1906
      2018
    • Length
      46 m
      70 m
    • Height
      7 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      25 m
      39 m
    • Wing loading
      331 kg/m2
      498 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
      92024 kg
      138036 kg
    • Max. takeoff weight (Gross weight)
      196800 kg
      295200 kg
    • Loaded weight
      194000 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
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      2647 km/h
      3971 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
      141600 l
      212400 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
      614 kN/kg
      922 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      403 kN
      605 kN
    • Service ceiling
      18880 m
      28320 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5520 km
      8280 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
      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
      600000000 USD
      750000000 USD

North American Aviation XB-70 Valkyrie

TypeAircraft
Company

North American Aviation

Scheme

Integrated

Monoplane

Geometry
Length (m)
1.9
 
57.6
88.7
Height (m)
0.6
 
9.1
50.1
Wings
Wingspan (Beam) (m)
0.1
 
32
95
Wing loading (kg/m2)
3.1
 
414.7
829
Weights
Empty weight (kg)
8
 
115,030
276,800
operating empty weight
Max. takeoff weight (Gross weight) (kg)
154
 
246,000
575,000
Loaded weight (kg)
5
 
242,500
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
3,309
28,165
Fuel
Fuel Capacity (l)
23
 
177,000
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Afterburning thrust (kN/kg)
29.4
 
768
980
6 powerplants 128 kN each
Thrust (kN)
1.5
 
504
1,914
6 powerplants 84 kN each
Performance
Service ceiling (m)
0.6
 
23,600
161,544
Range (Ferry range) (km)
4
 
6,900
40,700
on combat mission
Stat
Number built (qt)
0
 
2
43,000
Price (USD)
41.5
 
750.0 million
750.0 million
Introduction 1964
First flight 21.09.1964
Stop production 04.02.1969

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