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Wright Company Flyer (1903)
Military
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Bell Textron X-1
Military
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|---|---|---|
| Quick facts | ||
| Manufacturer | Wright Company | Bell Textron |
| Type | Experimental & historic pioneers | Experimental & historic pioneers |
| Origin | 🇺🇸 United States | 🇺🇸 United States |
| First flight | 1903 | 1946 |
| Status | Retired | Retired |
| Units built | 1 | 3 |
| Unit cost | — | — |
| Dimensions | ||
| Length | 6.43 m | 9.40 m |
| Wingspan | 12.29 m | 8.50 m |
| Height | 2.74 m | 3.30 m |
| Wing area | 47.4 m² | 12.0 m² |
| Weights & fuel | ||
| Empty weight | 274 kg | 3,175 kg |
| Max. take-off weight | 340 kg | 5,557 kg |
| Performance | ||
| Max. speed | 48 km/h | 1,541 km/h |
| Max. Mach | — | Mach 1.45 |
| Service ceiling | — | 21,900 m |
| Crew & capacity | ||
| Crew | 1 | 1 |
| Powerplant | ||
| Engines | 1 | 1 |
| Engine type | — | — |
| Engine model | Wright 4-cylinder inline (driving two propellers by chains) | Reaction Motors XLR11-RM3 four-chamber rocket |
| Thrust (each) | — | 26.7 kN |
| Power (each) | 9 kW | — |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.