| Type | Aircraft | |
| Company | Grumman Aerospace Corporation | |
| Scheme | Monoplane Midwing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
16.6
88.7
|
|
| Height (m) |
0.6
4.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
49.2
925
|
|
| Wingspan (Beam) (m) |
0.1
16.2
95
|
|
| Weights | ||
| Empty weight (kg) |
8
11,625.6
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
27,499.5
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
pilot, bombardier/navigator |
| Hardpoints (qt) |
1
5
2,576
|
4 wing and 1 fuselage |
| Speeds | ||
| Max. Speed (km/h) |
25
1,040
28,165
|
|
| Сruise Speed (km/h) |
52
774
3,087
|
|
| Power | ||
| Thrust (kN) |
1.5
82.8
1,914
|
2 powerplants 41,4 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
12,374.9
161,544
|
|
| Range (Ferry range) (km) |
4
5,222
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
2,322.6
36,000
|
|
| Stat | ||
| Number built (qt) |
0
693
43,000
|
|
| Price (USD) |
41.5
43.0 million
750.0 million
|
|
| Introduction | 1960 | |
| First flight | 19.04.1960 | |
| Stop production | 28.04.1993 | |
