Ir al contenido

Lockheed XC-35

Civilian
Lockheed XC-35

Imagen: Wikimedia Commons

The Lockheed XC-35, which first flew in 1937, was an experimental pressurized transport exploring high-altitude commercial operations. Its six-crew configuration, 11.8-meter fuselage, 16.8-meter wingspan, and twin-engine design achieved 379.8 km/h while pioneering cabin pressurization technology.

Especificaciones

Función
Experimental
Origen
United States
Tripulación
6
Motores
2
Primer vuelo
1937
Longitud
11,8 m
Envergadura
16,8 m
Velocidad máxima
380 km/h