E2T provides specialized test solutions for liquid-fueled rocket engines and other critical systems to its customers in the space sector. In line with our customers' requirements, we develop custom test systems across a wide range, from cold flow tests to strength and lifespan tests. Through turnkey test facility installations, we maximize the reliability, performance, and durability of rocket engines and space systems.

The success of space missions depends on the flawless operation of each component. Therefore, we design and install advanced test systems to measure critical parameters of liquid-fueled rocket engines, such as thrust measurement, combustion efficiency, vibration, and shock resistance. With our developed E2T Control Suite software, we automate your test processes and provide high-precision data acquisition and analysis capabilities. This ensures the repeatability and reliability of your tests.

Cold Flow Test Systems

Cold flow test systems are critical systems used in the development of liquid-fueled spacecraft to enhance the reliability of the engine. In these systems, no ignition is performed; instead, critical components such as the engine, tank, lines, and valves are subjected to individual or combined performance tests. In cold flow test systems, fuel and oxidizer system validations, leakage tests, pressure tests, turbo pump performance tests, and[…]
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Static Fire Testcell

Static firing test systems for spacecraft with liquid propulsion engines are critical test infrastructures used to verify the performance, reliability, and design of the engines. These tests can be conducted in both horizontal and vertical configurations. Each configuration serves different purposes and enables the collection of different data. The test stands and subsystems used for static firing tests are designed considering high pressure, high temperature, vibration, and[…]
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Thermal Shock Test System

In aviation and spacecraft engines, coatings are generally applied to relevant components to prevent deformations caused by high temperature, low temperature, wear, and oxidation-sulfidation conditions. The first of these is Thermal Barrier Coatings (TBC), which are used to reduce surface temperatures and minimize thermal stresses in components located in high-temperature areas such as the combustion chamber, turbine, and exhaust sections. TBC coatings are typically made of[…]
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