Tests under high temperature and high pressure conditions, including an annular combustor for aircraft jet engines

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Department Aviation Technology Directorate
Air supply units Pre-stage compressor: two 720 kW units, one 1,140 kW unit, one 2,240 kW unit, one 930 kW unit
Post-stage compressor: one 10,000 kW unit
Standalone operation test (test using post-stage compressor only) Maximum pressure: 0.8 Mpa
Maximum air temperature: 673 K
Maximum air flow rate: 8.5 kg/s
Series operation test (test using two-stage operations, a pre-stage compressor and post-stage compressor) Maximum pressure: 1.8 Mpa
Air temperature: 753 K
Maximum air flow rate: 18.5 kg/s
Year of completion Repairs in FY 2006 (constructed in FY 1975)
Fees Standalone operation test: 81,037 yen/hour (Current as of April 1, 2022)
Series operation test: 257,450 yen/hour (Current as of April 1, 2022)

*The usage fee above includes the general management fee.
*The usage fee above does not include technical fees and consumption tax. These fees will be charged separately.
*The usage fee above does not include required support fees, such as for operations. These fees will be charged separately depending mainly on the test details.
*The usage fee is calculated each fiscal year. In addition, prices may be revised without notice midway through the fiscal year. Inquire using the form below for details.

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