Testing gas turbine combustors and other equipment under high pressure conditions
Research mainly of combustion performance, exhaust characteristics, and cooling performance
|Department||Aviation Technology Directorate|
|Air supply units||Two 720 kW units; motor driven multi-stage centrifugal compressor|
|Sample section||Inlet air pressure: 0.11 to 1 Mpa
Inlet air temperature: 400 to 1,200 K
Inlet airflow volume: 0.4 to 3.6 kg/s
|Year of completion||FY 1982|
|Fees||29,307 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.