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In April 1942, the US Army Air Force was conducting flight testing of experimental liquid propellant units developed by the Air Corps Jet Propulsion Research Project at the California Institute of Technology to determine their effects on reduction of takeoff run, stability and control, high speed performance, blast effects, and reliability. The units were found to reduce takeoff distance by approximately one-third and increase maximum speed by approximately 40 miles per hour. However, improvements were recommended in terms of jet installation. In January 1943, flight tests were conducted by the US Army Air Force on Model AL-1000 liquid propellant jet units developed by Aerojet Engineering Corporation based on the April 1942 testing. The Aerojet units successfully reduced takeoff distance and increased flight velocity, as well as allowing for quick and easy servicing and or unit replacement. Aerojet Engineering Corporation began producing these different models of these units for the US Army Air Force subsequent to this testing.