| Type | Aircraft | |
| Company | Bell Aircraft Corporation | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
11.5
88.7
|
|
| Height (m) |
0.6
3.6
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
24.3
925
|
|
| Wingspan (Beam) (m) |
0.1
9.8
95
|
|
| Weights | ||
| Empty weight (kg) |
8
5,613.2
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
11,299.0
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
3,370
28,165
|
|
| Power | ||
| Thrust (kN) |
1.5
67
1,914
|
1 powerplant at sea level |
| Performance | ||
| Service ceiling (m) |
0.6
38,465.8
161,544
|
|
| Stat | ||
| Number built (qt) |
0
2
43,000
|
|
| Introduction | 1952 | |
| First flight | 18.11.1955 | |
| Stop production | 27.09.1956 | |
