| 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 | |
