| Manufacturer |
Bréguet Aviation |
Cox-Klemin |
| Description |
The Breguet Type I was an experimental aircraft built in France in 1909. |
The Cox-Klemin XA-1 was a 1920s American air ambulance biplane designed and built by the Cox-Klemin Aircraft Corporation for the United States Army Air Service, only two prototypes were built. |
| First Flight |
1909-06-28 |
1923-01-01 |
| Designer |
Louis Breguet |
Cox-Klemin |
| Length (m) |
9.15 |
9.144 |
| Cockpit Crew |
|
2 |
| Max Speed (km/h) |
60 |
194.7306 |
| Capacity Description |
|
2 litters |
| National Origin |
France |
United States of America |
| Number Built |
1 |
2 |
| Powerplant Description |
1 × Renault 50/60 hp, 45 kW (60 hp) each |
1 × Liberty L-12A V-12 liquid-cooled piston engine, 313 kW (420 hp) each |
| Primary Users |
|
United States Army Air Service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Breguet_Type_I |
en.wikipedia.org/wiki/Cox-Klemin_XA-1 |
| Flat Wing Span (m) |
13.7 |
13.4112 |
| Flat Wing Area (m²) |
40 |
|
| Aircraft Engine |
Renault 50/60 hp |
|
| Number of Engines |
1 |
1 |