| 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 | |
