We conducted a feasibility study containing concept design (predicting the state(temperature,flow rate) of seperate altitude-exhaust gas based on the thrust 30,000 lbf class engine, determining the air condition (temperature, pressure) supplied to seperate altitude engine, determing the exhaust gas cooling way). And based on this, we’ve created a bid proposals including creating standard of technical specifications for equipment, expense statements, schedules.


AETF feasibility test facility