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Authors
Modal analysis of a spacecraft solar panel
Kryuchkov A.N., Safin A.I., Ermilov M.A., Vidyaskina A.N., Igolkin A.A., Ye. V. Shakhmatov Y.V.
Experimental and analytical determination of the elastic characteristics of layered woven composites
Komarov V.A., Pavlov A.A., Pavlova S.A.
Research vibrational fatigue properties of forward wings bay MPKM
Postnov V.I., Postnova M.V., Mantusova O.Y.
Forecasting low-cycle fatigue life of gas-turbine engine parts by the method of equivalent tests for specimens with stress concentrator under extension-compression
Bukatyy S.A., Pakhomenkov A.V., Solntsev G.A., Bukatyy A.S.
Resistance of products made of steel 20GL to sulfide stress corrosion cracking
Blazhnov N.M., Borisenkova E.A., Khardin M.V.
Dataware of virtual lab for gas turbine engine testing
Rybakov V.N., Kuzmichev V.S., Kulagin V.V., Krupenich I.N., Fedorov D.V.
Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines
Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.
Training experiment at forecasting of quality and reliability of soldered joints of electronic assemblages
Shumskikh I.Y., Tyulevin S.V.
Numerical and experimental study of the strength of fabric carbon-epoxy composite structures
Komarov V.A., Kishov E.A., Charkviani R.V., Pavlov A.A.
Post-operation state and extension of service life of compressor blades of the gas-turbine power plant GTE-45-3
Tarasenko Y.P., Berdnik O.B., Tsareva I.N.
Authenticity of the vibration tests. Diagnosis and prediction of fatigue failure
Ovchinnikov I.N., Ermishkin V.A.
Analysis of stress distribution in the dangerous section area of specimens with fillets under bending using the finite-element modeling method
Vakuljuk V.S.
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.
Experimental studies of the components of high-frequency ion engine RD0310
Kazbanov A.A., Dronov P.A., Spivak O.O., Derkachev A.B.
Testing of combined air-rocket engine mak-up with pulsing combustion chamber
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Mathematical modeling of a controlled electromechanical actuator for special assembly and coupling equipment
Nosov A.S.
Flight development tests and attempted operation of «AIST» small satellites
Kirilin A.N., Tkachenko S.I., Salmin V.V., Semkin N.D., Papkov A.P., Abrashkin V.I., Tkachenko I.S., Zheleznov Y.E., Galaeva E.Y.
Research of the validity of forecasting low cycle durability of gas turbine engine parts based on Manson’s equation
Porter А.M., Bukatyi S.A., Leshin D.P.
Method of production testing of electronic parts
Nasedkin A.V., Tyulevin S.V., Piganov M.N.
Method of production testing of electronic parts
Nasedkin A.V., Shumskikh I.Y.
Dynamic tests of probes for measurement of pulsations pressure at the raised average pressure
1 1., 1 1., 1 1., 1 1.
Analysis of contact interaction of polymer honeycomb core and CFRP base layers in sandwich-core constructions
Pavlova S.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.
Evaluation of low cycle fatigue based on the use of Coffin-Manson dependence under zero-to-“soft” loading cycle
Pavlov V.F., Kirpichyov V.A., Kocherova E.E., Zlobin A.S.
Pilot study of frequency characteristics of an acoustic probe for measuring pressure pulsations in the gas turbine engine inlet device
Ivanenko V.N., Alexandrova T.G., Dyagileva E.C., Gimadiyev A.G., Bystrov N.D.
Development of thruster chamber operating on oxygen-hydrogen fuel
Salich V.L.
On the development of experimental methods in research of folded core type z-crimp on the transverse compressive test strength
Dvoeglazov I.V., Khaliulin V.I.
Development liquid roket engine on component fuel liquefied natural gas and oxygen for reusable space launching systems
Efimochkin A.F., Khrisanfov S.P., Golubyatnik V.V., Kafarena P.V., Yeliseyev A.V.
Increase durability of gas turbine disks
Nikishov O.V., Krutsilo V.G.
Investigation of extreme opportunities of stand supporting systems
Samsonov V.N., Kozyreva M.S., Cherevan A.A.
Methodological support for the training of UAV designers and operators
Lukyanov O.E., Zolotov D.V.
Development of the active gas generator for high altitude firing test benches
Salich V.L.
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.
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.
Results of hot tests of an oxygen preburner of a liquid-propellant engine 11D58MF
Barsukov O.A., Strizhenko P.P.
Stand for testing turbocharger rotor
Antipov V.A., Lazutkin G.V., Andrianov S.V., Velmin S.A.
Calculation methodology of intermittent burning chamber main parameters
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Experimental researches of possible low-thrust rocket adaptation developed by FSUE R&DIME for bipropellant MON-3+MMH providing tolerable thermal state thrusters
Beshenev Y.A., Buldashev S.A., Kazankin F.A., Lemskiy N.V., Semkin Y.V.
The devices for the diagnosis and control of turbine blades deformative condition during operation
Danilin A.I., Chernyavskiy A.G., Kapustin A.S.
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.
Problematic issues of assessing the strength of axisymmetric parachute systems by conducting breakdown tests in flight experiments
Ivanov P.I., Kurinnyy S.M., Krivorotov M.M., Shmerova G.V.
Development of intelligent peripheral devices of control and emergency protection systems for ground testing of liquid-propellant rocket engines
Volnukhin O.A., Liseykin V.A., Tozhokin I.A., Churin M.N.
Early detection of vibration behaviour of aircraft engine multistage axial compressor in pre-surge states during rig testing
Khorikov A.A., Danilkin S.Y., Mazikina T.I.
Computer-aided system of virtual gas turbine engine testing
Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Ostapuk Y.A., Filinov E.P.
Increasing the equivalence of realize full scale tests with the influence of geometrics parameters of the load system
Kulikov E.N.
Instrument to measure material resistance to thermo-mechanical fatigue
Tikhomirova E.A., Azizov T.N., Sidokhin E.F.
The machine and methods of tribotehnical tests of materials
Ibatullin I.D., Zhuravlev A.N., Utjankin A.V., Galljamov A.R., Neyaglova R.R.
Analysis of the results of fatigue tests of cylindrical specimens with fillets using the method of finite element modeling
Vakulyuk V.S.
Improvement of fretting wear resistance of blade root made of polymer composite material
Karimbayev T.D., Afanasiev D.V., Matyukhin D.V., Orlov M.A.
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.
Engineering design and experimental research of non-metallic parts and components of the hot section of the advanced gas turbine engine
Karimbayev T.D., Mezentsev M.A., Ezhov A.J.
Investigation of the vibration behavior of a gas turbine engine in icing conditions
Danilkin S.Y., Teleshev V.A.
Installation for strengthening local thermoplastic turbulent disc
Krutsilo V.G., Nikishov O.V.
The new testung method of coatings on high-temperature alloys
Tikhomirova E.A., Sidokhin E.F.
Improving the quality parameters of serial debug two spool mixed flow turbofan
Volik A.A., Gumerov K.S., Khabibullin R.Z., Khayrullin R.B.
Unit impulse input tests of a system of the «Frigate» upper-stage rocket
Mikhalenkov N.A., Yermakov V.Y., Utkina Y.I.
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.
Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate
Kocherova E.E.
Application of simulation modelling in static tests of space-rocket vehicles
Grebnev D.N., Duplihin V.K., Zuperman J.A., Aistov A.I., Kukushkin V.E.
Experimental design of a device for bird strike bench tests of non-rotating fan blades
Shorr B.F., Matsarenko V.S., Serebryakov N.N.
Analysis of the results of thermal cycic tests using TC-maps and problems of investigating thermal fatigue of materials
Tikhomirova E.A., Sidokhin E.F.
Design of reinforced specified fatigue life capability airframe panels containing notches
Bespalov V.A.
Numerical and experemental investigation of the dynamics of light multipurpose helicopter ditching
Mikhailov S.A., Nedelko D.V., Mukhametshin T.A., Belyaevskiy A.N., Gontsova L.G.
Creation of the technique of he delivery influence on working process in the LRE chamber with expulsion propellant supply
Shnyakin V.N., Kovalenko A.N., Kovalenko V.N., Rod'kin A.V., Bochev E.N., Makoter A.P., Blishun Y.V.
Tests of tubing made of aluminum alloy 1953T1 with wear-resistant thread-lined coats
Ivanova A.V.
Design of experiments for verification of computational life prediction methods
Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.
Conducting functional control of field-programmable gate arrays
Ogurtsov A.A.
Method of accelerated test research soldered joints surface mount devices
Nasedkin A.V.
Application of the invariant plastic flow theory for mathematical modeling of the processes of testing specimens under complex elastic-plastic deformation
Temis Y.M., Alkhimov D.A., Martynova A.D.
Perfection of methods of conducting resonance tests of rotor blades being part of the engine
Khorikov A.A., Danilkin S.Y., Redkin D.A.
Life testing of pipeline elements
Boltenkova O.M., Davydov O.Y., Yegorov V.G.
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.
Methodical features of vibration tests of rotating blades using dynamic spin rigs
Nozhnitsky Y.A., Fedina Y.A., Shadrin D.V.
Assuring the durability of transport aircraft structure in multipurpose use based on the results of endurance and flight tests
Fomichev P.A., Kleptsov V.I.
1 - 75 of 75 Items

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