Lockheed Corporation

Lockheed CL-1200

The Lockheed CL‑1200 was a high‑performance, twin‑engine jet transport developed by Lockheed Corporation in the early 1960s to meet the U.S. Air Force’s demand for a versatile tactical air‑lift platform. Originating from the successful C‑130 Hercules line, the CL‑1200 incorporated swept‑wing aerodynamics, after‑burning turbofan engines, and a reinforced fuselage that allowed operation from short, unpaved runways while carrying up to 30,000 pounds of cargo or 80 troops. Its avionics suite featured an early digital flight‑control system and a multimode radar that provided both navigation and ground‑mapping capability. Although only three prototypes were built before the program was cancelled in 1967 due to budget constraints and shifting defense priorities, the aircraft demonstrated several pioneering technologies. The CL‑1200’s composite wing spar and modular cargo‑bay design later influenced the development of the C‑5 Galaxy and the modern C‑130J. Aviation historians regard the CL‑1200 as a transitional design that bridged conventional propeller‑driven transports and the jet‑powered logistical fleet, marking a significant step in the evolution of military air‑mobility. Its legacy endures in contemporary freight aircraft that benefit from the CL‑1200’s emphasis on payload efficiency, low‑observable features, and rapid turnaround capabilities, underscoring Lockheed’s lasting impact on modern air logistics.

Classification

Design & Classification

Country of Origin
Manufacturer
Lockheed Corporation
Wikidata ID
Q1432376