Type | Aircraft | |
Company | Grumman Aerospace Corporation | |
Scheme | High wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
17.0
88.7
|
|
Height (m) |
0.6
5.0
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
41.8
925
|
swept |
1.1
43.4
925
|
spread | |
Wingspan (Beam) (m) |
0.1
11.2
95
|
swept |
0.1
15.4
95
|
spread | |
Weights | ||
Empty weight (kg) |
8
9,264.6
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
16,079.9
575,000
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
1,100
28,165
|
|
Сruise Speed (km/h) |
52
1,017
3,087
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.2
2.1
|
|
Thrust (kN) |
1.5
30.2
1,914
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
13,960
161,544
|
|
Range (Ferry range) (km) |
4
2,670
40,700
|
|
Stat | ||
Number built (qt) |
0
1
43,000
|
|
Introduction | 1952 | |
First flight | 19.05.1952 |