Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
The major improvement of JAXA's ground-level enclosed jet engine test facility was made in 2006 & 2007 Japan Fiscal Year. This test facility was constructed in 1976 with the capability of 100 kN thrust level turbofan engine testing for the research and development project of Japan's first high-bypass-ratio turbofan engine "FJR710". This test facility was improved to make it possible to conduct various tests which were necessary to verify the technology developed in the R&D on clean engine technology project carried forward by JAXA, and to support the development and qualification tests for the commercial engines domestically developed in the near future. The major improvement includes the improvement of the test cell air flow quality, the renewal of the thrust mount system, and the upgrade of the measurement system and data acquisition, processing & monitoring system. This memorandum describes the summary of the improvement and the updated test facility specification.