Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      25 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
      534 kg
      802 kg
    • Max. takeoff weight (Gross weight)
      944 kg
      1416 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      3 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      108 km/h
      162 km/h
    • Сruise Speed
      108 km/h
      162 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
      72 hp
      108 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2487 m
      3731 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      617 km
      927 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
      97 m/min
      147 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
      615 qt
      923 qt
    • Price
      6000 USD
      9000 USD

Curtiss-Robertson Airplane Manufacturing Company C-10 Robin

TypeAircraft
Company

Curtiss-Robertson Airplane Manufacturing Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
7.8
88.7
Height (m)
0.6
 
2.4
50.1
Wings
Wing area (m2)
1.1
 
20.7
925
Wingspan (Beam) (m)
0.1
 
12.5
95
Weights
Empty weight (kg)
8
 
667.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,180
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
2
400
Speeds
Max. Speed (km/h)
25
 
135
28,165
Сruise Speed (km/h)
52
 
135
3,087
Power
Total Power (hp)
0.4
 
90
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,109.0
161,544
Range (Ferry range) (km)
4
 
772
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
121.9
36,000
Stat
Number built (qt)
0
 
769
43,000
Price (USD)
41.5
 
7,500
750.0 million
Introduction 1928
First flight 07.08.1928

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