| Manufacturer |
General Dynamics |
| Description |
The General Dynamics X-62 VISTA ("Variable Stability In-flight Simulator Test Aircraft") is an experimental aircraft used since 1992 by the United States Air Force (USAF). |
| First Flight |
1992-04-01 |
| Designer |
General Dynamics |
| Type |
Experimental aircraft |
| Length (m) |
14.8 |
| Height (m) |
4.8 |
| Cockpit Crew |
2 |
| Max Speed (km/h) |
2172.615 |
| Max Ceiling (m) |
15240 |
| Rate of Climb (m/s) |
254 |
| Number Built |
1 |
| Powerplant Description |
1 × General Electric F110-GE-100 afterburning turbofan |
| Primary Users |
United States Air Force |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/General_Dynamics_X-62_VISTA |
| Flat Wing Span (m) |
9.8 |
| Flat Wing Area (m²) |
27.8709 |
| Aircraft Engine |
General Electric F110 |
| Number of Engines |
1 |