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 |