RI-062
Infrastructure
Description
Dedicated for testing and development of the small turbine engine combustion chambers. According to requirements the test rig can be scaled. First design was built for overpressure 5 bar with air flow of 1,8 kg/s.
Main technical characteristics
Maximum rotating speed
Maximum pressure
Maximum massflow rate, air/fuel-ratio
Maximum temperatures
Measurement instruments2
Comment
PropComb
Contact Information
Prague (Czech Republic)