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Description
| Notes: TWO-PLACE, high performance sailplane to be used for navy test pilot training. | ||
| Manufacturer: | Schweizer/Lockheed | |
| Base model: | X-26 | |
| Designation: | X-26 | |
| Version: | A | |
| Designation System: | U.S. Air Force | |
| Designation Period: | 1948-Present | |
| Basic role: | Research | |
Specifications
| Length: | 26' 9" | 8.1 m | |
| Height: | 9' 3" | 2.8 m | |
| Wingspan: | 57' 1" | 17.4 m | |
| Wingarea: | 180.0 sq ft | 16.7 sq m | |
| Empty Weight: | 857 lb | 388 kg | |
| Gross Weight: | 1,430 lb | 648 kg | |
Propulsion
| No. of Engines: | 1 | ||
| Powerplant: | Continental O-200-A | ||
| Horsepower (each): | 100 | ||
Performance
| Max Speed: | 158 mph | 254 km/h | 137 kt |
| Ceiling: | 18,500 ft | 5,638 m | |
Known serial numbers
