Flex System provides system solutions to test the functionality and performance of space launch vehicles using liquid fuels such as kerosene and methane. Liquid-fueled launch vehicle test systems are categorized into systems that test the combustor and turbopump, the core components of the engine; ground and high altitude simulated combustion test systems that simulate the conditions under which the launch vehicle burns outside of the atmosphere; and systems for controlling and instrumenting each stage propulsion test.
Flex System provides solid fuel test system design and build solutions. Test systems for solid-fueled space launch vehicles and large unguided and guided weapons are categorized into ignition, explosion, and combustion systems.
We provide solutions for building a comprehensive measurement system for test facilities that test the combustion performance, temperature, pressure, flow, vibration, shock, etc. of the combustor, a key component of a space launch vehicle engine.
We provide a solution for building a comprehensive measurement system for a test facility that tests the operation characteristics and compression performance of turbopumps, the heart of a launch vehicle engine, rotating at high pressure and high speed.
We provide a solution for building a comprehensive instrumentation system for a test facility that simulates the operation and combustion performance of space launch vehicle first, second, and third stage engines by simulating ground (sea level altitude) and high altitude (high altitude vacuum environment).
We provide a solution for building an integrated control and measurement system for the propulsion test facility that conducts water flow and combustion tests to verify the performance of each stage of the launch vehicle.
We provide solutions for building an integrated control and measurement system that controls test facilities during ignition, combustion, and explosion tests of solid-fueled space launch vehicles and large unguided/guided weapons, and acquires and stores pressure, thrust, temperature, strain, and ICP data from various sensors.
