Thrust Measurement Testcells are specialized systems used to measure the thrust output of turbojet and turbofan engines. Since these engines are primarily designed to generate thrust, such testcells are commonly employed during the initial testing phases of engine development. Through these systems, critical data—such as thrust levels, specific fuel consumption, vibration, temperature, and pressure—can be collected. This information provides engineering and design teams with essential insights into engine performance and optimization.

These testcells are not limited to thrust measurement alone; they also support a variety of additional tests, including engine endurance testing, water ingestion tests, and sand ingestion tests. They can be installed in open-air environments or, with minor modifications, integrated into the test chambers of Altitude Test Systems.

The design of a thrust measurement testcell involves consideration of numerous parameters, such as engine starting methods (pyrotechnic, windmilling, electric motor, APU, etc.), compatibility with mechanical, electronic, and software interfaces of engine accessories, the types of tests to be performed, the site where the testcell will be installed, and bellmouth characteristics.

Comprehensive support can be provided from the requirement-definition stage through commissioning, ensuring the development of high-precision thrust measurement testcells equipped with calibration interfaces, advanced data acquisition, control capabilities, and safety systems.