INDICATOR,THRUST,ENGINE TESTING - (US)
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.
Related Item Names for INC 32993 for US
STATOR,GENERATOR CONVERTER,SIGNAL DATA TRANSMITTER,PRESSURE INDICATOR,PRESSURE GAGE UNIT,ENGINE SYNCHROSCOPE,AIRCRAFT ENGINES GAGE,ABSOLUTE PRESSURE,DIAL INDICATING GAGE,PRESSURE,DIAL INDICATING INDICATOR,ELECTRICAL TACHOMETER TRANSMITTER,POSITION INDICATOR,RATE OF FLOW INDICATOR,RATE OF FLOW AND CONSUMPTION INDICATOR,POSITION INDICATOR,TORQUEMETER TRANSMITTER,RATE OF FLOW TRANSMITTER,RATE OF FLOW AND CONSUMPTION INDICATOR,SYNCHRONIZATION INDICATOR-TRANSMITTER,RATE OF FLOW CASE,DIAL INDICATING PRESSURE GAGE HOUSING,GAGE HOUSING,INDICATOR INDICATOR,RATIO,ENGINE PRESSURE INDICATOR,THRUST,ENGINE TESTING PARTS KIT,AIR FLOW REGULATOR MODIFICATION KIT,INSTRUMENTS AND LABORATORY EQUIPMENT GAGE AND VALVE ASSEMBLY COMPUTER,ENGINE CONVERTER,SIGNAL DATA SUBASSEMBLY INDICATOR,TEMPERATURE,FAN TURBINE INLET INDICATOR,MULTIPLE,ENGINE PARAMETERS DIAGNOSTIC UNIT,ENGINE INDICATOR SUBASSEMBLY,RATE OF FLOW INDICATOR SUBASSEMBLY,ELECTRICAL TACHOMETER TRANSMITTER SUBASSEMBLY,RATE OF FLOW INDICATOR SUBASSEMBLY,PRESSURE