Pulsed High-Power Systems for Geology and Geophysics.
Research of Problems in the Creation of Convertible Passenger and Transport Aircraft with Tilt-Rotor System.
The Fundamental Investigation and Experimental Working out of the Methods for the Creation of the Ecological Pure, High Temperature, Annulas Combustion Chamber for Turbojets
Design Studies of the Very Large Commercial Transport (VLCT) Aircraft with Non-traditional Layout Configurations.
Development of Experimental and Computational Methodology for Investigation of thermal Properties of Composite Materials Based on Inverse Problem Theory and Stochastic Approaches
Development of Experimental and Computational Methodology for Investigation of Thermal Properties of Composite Materials Based on Inverse Problem Theory and Stochastic Approaches
The Rocket Engine Jet Nozzle with High-Altitude Characteristics
Artificial Heart Based on the Pulsating Centrifugal Pump
Theoretical Investigation and Experimental Development of Methods of Building up Non-Toxic Combustion Chamber of Gas-Turbine Engine with Low Soot Formation in Combustion Liner
Small-Scale Ignition Unit for Simplification of Diesel Engines Start at Winter Conditions, Supplied by Gas-Dynamic Igniter with Supersonic Nozzle and Gas-Liquid Injector with Porous Insert
Thermal Diagnostics Technologies for Development, Verification and Emergency Prevention of Aerospace Structures
Power Plant Nozzle Cluster with Altitude Compensation
Development of a Low-Toxic Gas-Turbine Combustion Chamber Based on Plasma Assisted Fuel Combustion
Investigation of Plasma Technology for Nanostructure Layer Deposition
Promising Nanostructural Materials for Cryogenic Electrical Machines