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 |