Special Features:

Finish semi gloss black; output digital display; continuous 5 digit lighted numerical indication of engine thrust in pounds; accuracy +/- 10 lbs up to 10, 000 lbs and +/- 0.1% of reading above 10, 000 lbs; input signal source: summed output of 2 25, 000 lbs compression load cells; operation modes test or check, operate and range selector; adjustments: sampling rate, load cell zero balance, and range span calibration; operating temp 20 to 130 degrees f

Properties:

An engine testing instrument designed to reflect the forwardly directed reaction force produced by a high-speed jet of fluid discharged rearwards from a nozzle orifice (as in a jet plane or rocket). It designates in units of thrust, the thrust output of gas turbine or jet propulsion engines. This instrument is normally used on a stationary, mobile, or portable gas turbine engine test system.