Aerospace Testing Facilities available in India
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| Title of the Aerospace Test |
Pass-off Test for Aero Gas Turbine Combustor |
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| Name of the Organisation |
DRDO |
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| Name of theLab |
Gas Turbine Research Establishment - GTRE |
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| Place of the Lab |
Bangalore |
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| Category of Aerospace Test | Aerodynamic Test | |
| Sub-category of Aerospace Test | NA | |
| Year of Establisment | 1985 | |
| Test Applications | Ignition Test (above atmosphere pressure only) Iso-Thermal Test for Pressure Loss Measurement Non-uniformity temperature measurement |
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| Test Special Features | Combustor can be tested up to - 500 kPa inlet air pressure , pre-heat air temperature up to 550 K , air mass flow rate up to 15 kg/s. Combustor can be tested with Aviation Turbine Fuel and Diesel Fuel. The test facility is instrumented for 192 air pressure measurement, 192 air temperature measurement (K-type, N-Type and R-Type), 32 channel RTD measurement Reference Air Mass Flow measurement (Orifice Type) Underground ATF Fuel Storage 5000 Litters. |
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| Other Test Information | Electronic Pressure Scanner System Online Exhaust Gas Analyser System (UHC, CO2, CO, NOX, O2 species) Data Acquisition System ATF Fuel Pump |
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| Contact Person / Institution | The Director Gas Turbine Research Establishment (GTRE) Defence Research and Development Organization (DRDO) Ministry of Defence PO Box 9302, CV Raman Nagar Bangalore-560 093 E-mail : director@gtre.drdo.in Website:http://www.drdo.gov.in/drdo/labs/GTRE/English/index.jsp?pg=homebody.jsp |
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