USA - Naval aviation and armament
Grumman F11F (F-11) Tiger fighter
F11F-1 (F-11A) Tiger
| Modification | Purpose | Deliveries | Number of commissioned | Discarding | Differences from the previous modification |
| F11F-1 Short Nose, 1962 - F-11A | fighter - bomber | 3/1957 - 1957 | 41 | 4/1961 | Wright J65-W-6 engine (3386 / 4764 kgf) |
| F11F-1 Long Nose, 1962 - F-11B | 1957 - 12/1958 | 157 | 4/1961 | lengthened hull, J65-W-18 engine (3538 / 4990 kgf) |
| Modification | F11F-1 Long Nose (F-11B) |
|
Wing span, m |
9.68 |
|
Length, m |
14.30 |
|
Height, m |
4.05 |
|
Wings area, m2 |
23.22 |
|
Empty mass, kg |
6090 |
|
Full flying-off mass, kg |
10922 |
| Engine | 1 Wright J65-W-18 |
|
Force, kgf |
3538 / 4990 |
| Maximal speed, km/h | 1.1 Ì |
| Cruise speed, km/h | |
| Flying range, km | 2237 |
| Vertical speed, m/s | 26.1 |
| Maximal altitude, m | 12770 |
| Complement | 1 |
| Armament | 4 20-mm guns, 1816 kg of combat load on 4 wing points (4 Sidewinder AAM or 4 Bullpup ASM or 4 127-mm HVAR rockets or 76 70-mm FFAR rockets or 4 454-kg bombs) |
F11F-1 (F-11B) Tiger
© Ivan Gogin, 2008