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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.
Solicitation | Description | Qty | UOM | Close Date |
---|---|---|---|---|
SPE7M120T291K | Indicator, Thrust, En | 1 | EA | 04/23/2020 |
SPE7M120T332K | Indicator, Thrust, En | 1 | EA | 05/04/2020 |
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