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Lockheed XC-35

Civilian
Lockheed XC-35

Immagine: 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.

Specifiche tecniche

Ruolo
Experimental
Origine
United States
Equipaggio
6
Motori
2
Primo volo
1937
Lunghezza
11,8 m
Apertura alare
16,8 m
Velocità massima
380 km/h