
Zhukovsky National Research Center patented a nacelle for a turbofan engine with a bypass ratio of 6-7
The design is calculated for an air flow through the gas generator of 1.15 kg/s

The design is calculated for an air flow through the gas generator of 1.15 kg/s

The new scheme provides for yaw control retention

TsAGI began testing the behavior of the long nose of the airliner during takeoff and landing for the first time

GosNIIAS: there will be no frontal glazing in the aircraft

Compact GTE received an adaptive temperature control system