| Type | Aircraft | |
| Company | Consolidated Vultee Convair | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
9.8
88.7
|
|
| Height (m) |
0.6
7.0
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
33.0
925
|
|
| Wingspan (Beam) (m) |
0.1
8.4
95
|
|
| Wing loading (kg/m2) |
3.1
186
829
|
|
| Weights | ||
| Empty weight (kg) |
8
5,052.6
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
7,370.9
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
763
28,165
|
at 4600 |
| Сruise Speed (km/h) |
52
720
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
5,097.9
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
11,440
161,544
|
|
| Range (Ferry range) (km) |
4
805
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
3,041.9
36,000
|
|
| Propellers | ||
| Propellers (qt) |
1
2
8
|
contra-rotating |
| Prop blade number (qt) |
1
3
8
|
per propeller |
| Combat | ||
| Guns (qt) |
1
4
18
|
20mm (0.79 in) cannon |
| Rockets (qt) |
1
48
76
|
2.75 in (70 mm) Mk 4 Folding-Fin Aerial Rockets or |
| Stat | ||
| Number built (qt) |
0
3
43,000
|
only 1 flown |
| Introduction | 1954 | |
| First flight | 19.04.1954 | |
