The Aerothermodynamic Measurement System for Future Experimental and Operational Space Transportation Systems

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Scientific paper

In the frame of the German national technology program ASTRA an Aerothermodynamic Measurement System (AMS) was further developed. The system was originally designed and flight-qualified for use in the X-38 re-entry vehicle. The objective of the project was to extend the temperature range for application and the number of physical quantities, which can be measured. In addition the resulting system should be adaptable to a multiplicity of different thermal protection systems. This paper summarizes the most recent status of the new AMS design, development and qualification, including • a brief set of main requirements; • the system variants; • a conceptual system design overview; • the qualification program and test results; • and a look-out to potential applications.

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