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
NIC «Institut imeni Zhukovskogo»
Zhukovsky NIC developed a 4-engine aircraft with wingtip engines without kerosene
The new scheme provides for yaw control retention
Zhukovsky National Research Center created a gas turbine engine with self-regulating cooling without electronics
Compact GTE received an adaptive temperature control system
