Aircraft engine annular combustor test facility

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

Array

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: 170,155 yen/hour (Current as of April 1, 2026)
Series operation test: 548,470 yen/hour (Current as of April 1, 2026)

*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.