Type | Aircraft | |
Company | Grumman Aerospace Corporation | |
Scheme | Monoplane High wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
13.3
88.7
|
|
Height (m) |
0.6
5.3
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
46.1
925
|
|
Wingspan (Beam) (m) |
0.1
22.1
95
|
|
Weights | ||
Empty weight (kg) |
8
8,307.5
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
11,860.1
575,000
|
|
Loaded weight (kg) |
5
10,630
242,500
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
two pilots, two detection systems operators |
Speeds | ||
Ground Speed (km/h) |
96.6
450
1,500
|
|
Сruise Speed (km/h) |
52
240
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
2,476.3
320,000
|
|
Power | ||
Total Power (hp) |
0.4
3,050
60,000
|
2 powerplants 1525hp each |
Performance | ||
Service ceiling (m) |
0.6
6,705.6
161,544
|
|
Range (Ferry range) (km) |
4
2,170
40,700
|
|
Сombat radius (km) |
277
1,853
7,210
|
|
Endurance (h) |
0.0
9
150
|
|
Stat | ||
Number built (qt) |
0
1,284
43,000
|
|
Introduction | 1954 | |
First flight | 04.12.1952 |