Northrop YF-17A Cobra
| GENERAL DATA | |||
| Type |
Northrop YF-17A Cobra
|
||
| Manufacturer(s) | Nortrhop |
||
| Prototype first flight | 9 June 1974 |
Introduction | - |
| Produced | - |
Number built | 2 |
| Status | Retired |
Crew | 1 |
| DIMENSIONS | |||
| Length | 16.92 m |
Empty Weight | 9525 kg |
| Wingspan | 10.67 m |
Loaded Weight | 10433 kg |
| Height | 4.42 m |
Max takeoff weight | 13894 kg |
| Wing area | 33 m² |
Wing loading | 478,199 kg/m² |
| ARMAMENT | |||
| Guns | 1× 20 mm (0.79 in) M61 Vulcan
Gatling gun |
Ammunition Carried |
? |
| Other Armament | 5150 kg of load - 2 hardpoints:
2× AIM-9 Sidewinder missiles |
||
| POWERPLANT | |||
| Engine | 2 ×
General Electric YJ101-GE-100 turbojet
|
||
| Dry thrust | 4300 kgp (42 kN) each |
Thrust with afterburner | 6804 kgp (67 kN) each |
| Thrust/weight | ?
|
Fuel Capacity | ? kg |
| PERFORMANCES | |||
| Maximum Speed | Mach 2
(2120 km/h) at 12000 m |
Rate of climb | 250 m/s |
| Range | 4500 km |
Service ceiling | 15240 m |
| Sources | |||
| Wikipédia | aviationsmilitaires | ||
Drawings |
