Type | Aircraft | |
Company | Consolidated Vultee Convair | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
22.8
88.7
|
|
Height (m) |
0.6
8.2
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
75.9
925
|
|
Wingspan (Beam) (m) |
0.1
28.0
95
|
|
Rotors | ||
Rotor number (qt) |
1
3
8
|
|
Weights | ||
Empty weight (kg) |
8
11,541.7
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
26,372
575,000
|
|
Loaded weight (kg) |
5
18,370.5
242,500
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
2 or 3 flight deck crew |
Capacity passengers (per.) |
1
40
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
506.9
28,165
|
|
Сruise Speed (km/h) |
52
450.6
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
3,785.4
320,000
|
|
Power | ||
Total Power (hp) |
0.4
4,800
60,000
|
2 powerplants 2400 hp each |
Performance | ||
Service ceiling (m) |
0.6
4,877
161,544
|
|
Range (Ferry range) (km) |
4
3,650
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
462
36,000
|
|
Propellers | ||
Prop blade number (qt) |
1
3
8
|
|
Stat | ||
Number built (qt) |
0
1,181
43,000
|
|
Introduction | 1955 | |
First flight | 16.03.1947 |