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Development and research testing of a low thrust on gaseous-propellant rocket engine chamber
Musteikis A.I., Levikhin A.A., Kolosenok S.V.
Model of the turboprop engine reduction gear tooth harmonic spectral component
Sundukov A.E., Shakhmatov E.V.
Numerical study of possibility of reliable diagnostics of gas turbine engine by gasdynamic parameters using a linear mathematical model
Gerasimov A.B., Sundukov M.Y.
Investigation of the vibration behavior of a gas turbine engine in icing conditions
Danilkin S.Y., Teleshev V.A.
Discrete phase converters moving elements rotating units power units
Danilin A.I., Grechishnikov V.M.
Criteria of discrete phase control of blade working condition and their feasibility in systems of turbine driven set automatic control
Danilin A.I., Tchernyavsky A.Z.
Complex failure analysis of aero engine compressor blades
Sachin V.M., Tumanov N.V., Lavrentyeva M.A., Cherkasova S.A.
Perfection of methods of conducting resonance tests of rotor blades being part of the engine
Khorikov A.A., Danilkin S.Y., Redkin D.A.
Research of textural features for the diagnostics of nephrological diseases using ultrasound images
Gaidel A.V., Larionova S.N., Khramov A.G.
Methods and models of autonomous control over Earth remote sensing spacecraft survivability
Akhmetov R.N.
Inertial measuring units for future-generation aerospace products: fault-tolerance
Vodicheva L.V., Bel'skiy L.N., Parysheva Y.V., Lystsov A.A.
Thermal medical software hardware-based thermal imager COX CX - 320U
Davydov I.E., Agafonov A.N.
Diagnostics of computer modules of the Superjet-100 aircraft using the method of boundary scan
Grechishnyikov V.M., Kuritsky A.A., Manuilov I.Y.
Current state of the theory and practice of circuit wiring control and testing of the avionics of rocket fairings of middle-class launch vehicles
Koptev A.N., Gulyaev A.A.
Analysis of the accuracy of autonomous navigation of the space robot in the diagnosis of the technical condition of an orbital object
Golyakov A.D., Fominov I.V., Korolev S.Y.
Parameters transducers of the blade’s dynamic movements of turbounits based on nonlinear approximation of primary signals
Chernyavskiy A.Z., Danilin A.I., Danilin S.A.
Applied problems in the theory of diagnostic process for aircraft flight-navigation complexes
Koptev A.N., Kirillov A.V.
Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor
Posadov V.V., Remizov A.E.
The method of providing heat traceability of wireless devices at the stage of project
Uvaysov S.U., Yurkov N.K.
Flight-navigation complex diagnostics at the aircraft manufacture stage
Koptev A.N., Kirillov A.V.
Development of the criteria of analyzing the stress-strain state of gas turbine engine parts in the elastoplastic range
Bukaty A.S., Bukaty S.A.
The device for the determination of blades oscillation parameters based on nonlinear approximation of primary transducers signals
Danilin A.I., Chernyavskiy A.Z., Danilin S.A.
Mathematical model of the inline sensor based on matrix photodetector
Kornilin D.V.
Using the theory of dynamic analogies for modelling automated manufacturing systems
Gareyev A.M., Koptev A.N., Gareyev T.M.
Authenticity of the vibration tests. Diagnosis and prediction of fatigue failure
Ovchinnikov I.N., Ermishkin V.A.
Measurament of characteristics and spectral structure of laser plasma
Timchenko P.E., Marinin V.L.
Method of constructing diagnostic models of aircraft hydraulic systems in an analytic form
Kovalev M.A., Borodkin G.V., Khablo I.I.
Diagnostic methods and tools for condition-based maintenance of aircraft drives
Golovanov V.V., Vasilenko V.G., Zemskov A.A., Panov S.S., Emelianova A.A.
Identifying the boundaries of skin tumors by differential backscatter
Zakharov V.P., Kozlov S.V., Timchenko E.V., Timchenko P.E., Moryatov A.A., Bratchenko I.A., Taskina L.A.
Tooling system of express assessment of explosive military equipment objects after hitling effects
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