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 |