| Type | Aircraft | |
| Company | Grumman Aerospace Corporation | |
| Scheme | Monoplane Midwing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
14.3
88.7
|
|
| Height (m) |
0.6
4
50.1
|
|
| Wings | ||
| Wingspan (Beam) (m) |
0.1
9.6
95
|
|
| Wing loading (kg/m2) |
3.1
411
829
|
|
| Weights | ||
| Empty weight (kg) |
8
6,264.1
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
10,640.8
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Hardpoints (qt) |
1
4
2,576
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
1,170
28,165
|
at 11000 m |
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.5
2.1
|
|
| Afterburning thrust (kN/kg) |
29.4
46.7
980
|
|
| Thrust (kN) |
1.5
32.9
1,914
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
14,935.2
161,544
|
|
| Range (Ferry range) (km) |
4
2,050
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
4,968.2
36,000
|
|
| Combat | ||
| Guns (qt) |
1
4
18
|
20 mm (.79 in) Colt Mk 12 cannon, 125 rounds per gun |
| Stat | ||
| Number built (qt) |
0
200
43,000
|
|
| Introduction | 1954 | |
| First flight | 30.07.1954 | |
| Stop production | 1961 | |
