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    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      36 m2
      56 m2
    • Wingspan (Beam)
      0 m
      95 m
    • Wing loading
      187 kg/m2
      281 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
      3 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
      6273 kg
      9411 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      9496 kg
      14246 kg
    • Crew
      1 per.
      112 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
      533 km/h
      800 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      108 km/h
      163 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
      1211 l
      1817 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      11 hp/kg
      18 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
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      508 km
      763 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
      955 m/min
      1433 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
      3 m
      5 m
    • Prop blade number
      3 qt
      5 qt
    • Guns
      3 qt
      5 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

Grumman XTSF

Company

Grumman Aerospace Corporation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
14.1
88.7
Height (m)
0.6
 
4.9
50.1
Wings
Wing area (m2)
1.1
 
46
925
Wing loading (kg/m2)
3.1
 
234
829
3.1
 
234
829
Rotors
Rotor number (qt)
1
 
2
8
Weights
Empty weight (kg)
8
 
7,841.7
276,800
Loaded weight (kg)
5
 
11,871.0
242,500
Capacity
Hardpoints (qt)
1
 
2
2,576
450 kg capacity each
Speeds
Max. Speed (km/h)
25
 
666.3
28,165
at 5700 m
Stall Speed (km/h)
40
 
135.2
257.7
Fuel
Fuel Capacity (l)
23
 
1,514.2
320,000
Power
Power/mass (hp/kg)
0.0
 
14.3
22.1
Performance
Сombat radius (km)
277
 
635.7
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,194
36,000
Propellers
Prop diameter (m)
1.8
 
4.0
5.8
Prop blade number (qt)
1
 
4
8
Combat
Guns (qt)
1
 
4
18
.50-calibre machine guns
Stat
Number built (qt)
0
 
0
43,000
none

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