Aircraft engine annular combustor test facility
Tests under high temperature and high pressure conditions, including an annular combustor for aircraft jet engines
|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.