Lockheed Saturn

The Saturn (Model 75) was a small feeder airliner produced by Lockheed in the mid 1940s.


<sup>General characteristics

* Crew: Two
* Capacity: 14 passengers
* Length: 56 ft 6 in (15.69 m)
* Wingspan: 74 ft 0 in (22.56 m)
* Height: 19 ft 10 in (6.05 m)
* Wing area: 502 ft² (46.6 m²)
* Empty weight: 11,361 lb (5,153 kg)
* Loaded weight: 16,000 lb (7,257 kg)
* Powerplant: 2× Wright 744C-7BA-1 seven cylinder radial engine, 700 hp (522 kW) each

Performance

* Maximum speed: 198 kn (228 mph, 367 km/h) at sea level
* Cruise speed: 163 kn (187 mph, 301 km/h)
* Range: 522 nmi (600 mi, 965 km)
* Service ceiling: 26,500 ft (8,075 m)
* Rate of climb: 1,325 ft/min (6.7 m/s)</sup>