| Type | Aircraft | |
| Company | Grumman Aerospace Corporation | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
19.1
88.7
|
|
| Height (m) |
0.6
4.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
54.5
925
|
|
| Wingspan (Beam) (m) |
0.1
11.6
95
|
Swept |
|
0.1
19.6
95
|
Spread | |
| Wing loading (kg/m2) |
3.1
553.9
829
|
|
| Weights | ||
| Empty weight (kg) |
8
19,838
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
33,724.6
575,000
|
|
| Capacity | ||
| Hardpoints (qt) |
1
10
2,576
|
6× under-fuselage, 2× under nacelles and 2× on wing gloves |
| Speeds | ||
| Ground Speed (km/h) |
96.6
1,470
1,500
|
|
| Max. Speed (km/h) |
25
2,485
28,165
|
|
| Сruise Speed (km/h) |
52
870
3,087
|
|
| Landing Speed (km/h) |
68
250
270
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.9
2.1
|
|
| Afterburning thrust (kN/kg) |
29.4
241
980
|
2 powerplants 120,5 kN each |
| Thrust (kN) |
1.5
147.8
1,914
|
2 powerplants 73.9 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
15,200
161,544
|
|
| Range PTB (Ferry range) (km) |
720
2,960
10,000
|
|
| Dynamic Performance | ||
| Load factor from (G) |
2
7
9
|
|
| Rate of climb (m/min) |
1.9
13,716
36,000
|
|
| Combat | ||
| Guns (qt) |
1
1
18
|
20 mm (0.787 in) M61A1 Vulcan 6-barreled Gatling cannon, with 675 rounds |
| Stat | ||
| Number built (qt) |
0
712
43,000
|
|
| Price (USD) |
41.5
38.0 million
750.0 million
|
|
| Introduction | 1970 | |
| First flight | 21.12.1970 | |
| Stop production | 22.09.2006 | |
