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Experimental method for evaluating the balance of high-speed small-sized internal combustion engines
Rekadze P.D., Sychugov S.Y., Melentiev V.S., Rodionov L.V.
Bench tests of an electric engine-propeller group, as the first stage in the creation of a hybrid power plant
Sychev A.V., Ravikovich Y.A., Borisov D.A.
Conducting functional control of field-programmable gate arrays
Ogurtsov A.A.
Model of the turboprop engine reduction gear tooth harmonic spectral component
Sundukov A.E., Shakhmatov E.V.
Method of production testing of electronic parts
Nasedkin A.V., Tyulevin S.V., Piganov M.N.
About the probes for measuring pulsations of pressure in the flowing part gas turbine engines
Shorin V.P., Gimadiev A.G., Bystrov N.D., Ilinskij S.A.
Developing methods for electrical tests of onboard devices incorporated in spacecraft
Karasev A.A., Chuprinskiy I.I.
Results of hot tests of an oxygen preburner of a liquid-propellant engine 11D58MF
Barsukov O.A., Strizhenko P.P.
Experimental research of thermal yet influence of staff LTRE upon the construction models of airspace devices
Shustov S.A.
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.
Increase of the role of conformity assessment at the facilities controlled by the federal service on ecological, technological and nuclear supervision
Barvinok V.A., Naumov L.A., Dolgikh A.V.
The devices for the diagnosis and control of turbine blades deformative condition during operation
Danilin A.I., Chernyavskiy A.G., Kapustin A.S.
Test bench for investigation of thrusters intra-chamber working processes
Pervyshin A.N., Ryazanov A.I.
Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines
Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Fundamentals of optical measurements of informative components of complex movements
Nesterov V.N., Nesterov D.V.
Critical rotation frequency estimation of multispan rotors as rotors with elastic foundation
Petruhina N.P.
Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber
Silyutin M.V., Shustov S.A.
Investigation of the gas turbine engine combustion chamber workflow
Markushin A.N., Baklanov A.V.
Stand for testing turbocharger rotor
Antipov V.A., Lazutkin G.V., Andrianov S.V., Velmin S.A.
Increase durability of gas turbine disks
Nikishov O.V., Krutsilo V.G.
Characteristics of the sampling instrument for measuring emissions of an aircraft gas turbine engine
Okhlobystin A.V., Lyubimov R.V., Sokolova N.N.
Dataware of virtual lab for gas turbine engine testing
Rybakov V.N., Kuzmichev V.S., Kulagin V.V., Krupenich I.N., Fedorov D.V.
Procedure of estimating characteristics of angular velocity meter using the Kalman filter and Allan variance
Kutovoy D.A., Maslova O.I., Perepelkina S.Y., Tiunov Y.S., Fedotov A.A.
Increasing the equivalence of realize full scale tests with the influence of geometrics parameters of the load system
Kulikov E.N.
Test benches for researching the processes and operational development of low emission gas turbine engine combustion chambers
Markushin A.N., Baklanov A.V.
Procedure of assessing the error of the device for measuring mass-centering and inertial characteristics of nanosatellites using reference objects
Vasin P.V., Barinova E.V.
Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants
Silyutin M.V., Shustov S.A.
Modeling orbital tether system deployment with limitations on the deployment speed
Ishkov S.A., Filippov G.A., Xiaoye X.
Installation for strengthening local thermoplastic turbulent disc
Krutsilo V.G., Nikishov O.V.
Diagnostics of computer modules of the Superjet-100 aircraft using the method of boundary scan
Grechishnyikov V.M., Kuritsky A.A., Manuilov I.Y.
Comparison of mass properties of high- pressure cylinders with cryogenic fill for a throttle cooling system
Dovgjallo A.I., Sarmin D.V., Uglanov D.A.
Optimization of honeycomb sandwich floor panels made of polymer-matrix low-combustible composite materials based on high-strength carbon and glass fibers and adhesive binder
Komarov V.A., Kutsevich K.E., Pavlova S.A., Tyumeneva T.Y.
Analisys of experimental combustion chambers fire tests for LRE with cooling by liquid oxigen for "DM" type booster
Smolentsev A.A., Strizhenko P.P.
Calculation and experimental investigations on the efficiency of various ways of vibration damping of jet engine parts
Shorr B.F., Serebryakov N.N., Stadnikov A.N., Shadrin D.C., Rudenok E.S., Kanackin A.V., Bortnikov A.D.
Life testing of pipeline elements
Boltenkova O.M., Davydov O.Y., Yegorov V.G.
Particularity of thermal condition computation oF LRE with cooling by liquid oxygen
1 1.
On-stand emergency protection and control system for propulsion tests of «Soyuz-2-1B» launch vehicle
Liseykin V.A., Tozhokin I.A.
Verification of a design model and evaluation of a technique of manufacturing aircraft engine composite parts on the basis of dynamic tests
Zinin A.V., Arkhipov A.N., Kholobtsev D.P., Ravikovich Y.A., Shevjakov A.O., Kholmanova M.A.
Experiment-calculated research of the influence of the shot-peening strengthening upon the low-cycle fatigue of the gas turbine parts with the stress concentrator
Porter A.M., Bukaty S.A., Leshin D.P., Bukaty A.S.
Experimental design of a device for bird strike bench tests of non-rotating fan blades
Shorr B.F., Matsarenko V.S., Serebryakov N.N.
On the development of probes for measuring pressure pulsations in the gas-dynamic channel gas generator
Shorin V.P., Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A., Alexandrova T.G.
The integrated information model architecture for working out, manufacture and operation GTE together with its system of automatic control, the control and diagnostics
Kulikov G.G., Rizvanov K.A., Denisova S.S.
Design of experiments for verification of computational life prediction methods
Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.
Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster
Salich V.L.
Test verification of flow stabilizer calculated parameters provided flow stabilization of propellant in wide range of input parameters
Beshenev Y.A., Volkov A.V., Kazankin F.A.
Firing test stand pulse detonation low-thrust engines
Govorenkho G.S., Teterin D.P., Kotelnikhov D.S., Aliluev A.V., Aliluev S.V., Fedorets V.N.
1 - 46 of 46 Items

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