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Elaboration and testing of the algorithm which ensures an achievement of minimal deviation angle of flying model’s main centroidal axis of inertia during her counterbalancing in a sole correction flatness
Klyuchnikov A.V.
Features and modernization methods of thrust measurement devices for liquid rocket engine test stands
Begishev A.M., Zhuravlev V.Y., Torgashin A.S.
Automated stand for electrical testing and diagnostics of life characteristics of lithium-ion batteries
Kopylov E.A., Lobanov D.K., Mizrah E.A.
Analysis of the stress-deformed state of the prismatic support of the lever-grading device of test stands for liquid rocket engines
Begishev A.M., Zhuravlev V.Y., Nazarov V.P., Torgashin A.S.
Elaboration and testing of the algorithm which ensures an achievement of minimal deviation angle of flying model’s main centroidal axis of inertia during her counterbalancing in a sole correction flatness
Filonova M.M.
EVALUATION OF THE ANTENNA POINTING SYSTEM DISTURBING MOMENT IN THE EXPERIMENTAL PROCESS
Goncharuk A.V., Lukyanenko M.V., Raevsky V.A.
DETERMINATION OF DYNAMIC PARAMETERS OF THE DRIVE OF THE EXPERIMENTAL STAND FOR RESEARCH OF CARDAN TRANSFERS
Struchkov A.V., Kukushkin E.V., Eresko S.P., Eresko T.T.
Dynamical workbench for signature analysis and operating conditions of flywheel engine group of pointing and attitude control systems of spacecrafts
Synitskiy D.E., Murygin A.V.
NUMERICAL ALGORITHM FOR OPTIMIZATION OF A PROCESS OF CONICAL FLYING MODEL EQUILIBRATION ON A VERTICAL BALANCING STAND
Klyuchnikov A.V.
IMPROVEMENT OF THE METHOD OF CALCULATING THE UNIVERSAL JOINTS TRANSMISSION ANGLE WITH THE USE OF THEORETICAL AND EXPERIMENTAL STUDIES
Eresko S.P., Eresko T.T., Kukushkin E.V., Menovshikov V.A.
METHODS OF PREPARATION OF THE EXPERIMENT FOR INVESTIGATION OF UNIVERSAL JOINTS ON NEEDLE BEARINGS
Eresko S.P., Eresko T.T., Kukushkin E.V., Menovshikov V.A., Orlov A.A.
Automated control system of manipulator
Mirzaev R.A., Smirnov N.A.
AN APPROACH TO GROUND TESTING OF ROCKETS AND SPACE VEHICLES ON TRANSIENT PROCESSES BY COPRA-SPRING STAND
Bondarenko A.Y., Mitin A.Y., Tolchenov V.A., Eykhorn A.N., Yuranev O.A.
Development of disturbance moments definition method for working reaction flywheels assemblies installed on the special forces measuring stand
Denisova A.A., Tveryakov O.V., Britova J.A.
COMPARATIVE ANALYSIS OF STRUCTURES TEST APPARATUS FOR UNIVERSAL JOINT
Eresko S.P., Eresko T.T., Kukushkin E.V., Menovschikov V.A., Mikheev A.E.
TECHNOLOGICAL SUPPORT OF QUALITY DURING THE MANUFACTURE OF HYPERSONIC UNCONTROLLABLE FLYING MODELS
Ilinykh V.V., Klyuchnikov A.V., Lysykh A.V., Mihailov E.F., Timoshchenko A.G.
PLANNING OF EXPERIMENTS TO INVESTIGATE THE DRIVELINE ON NEEDLE BEARINGS
Kukushkin E.V., Eresko S.P., Eresko T.T., Menovshikov V.A., Khomenko I.I.
THE FEATURES OF PRODUCTION OF WAVEGUIDE-DISTRIBUTIVE SYSTEMS OF COMMUNICATION SPACECRAFTS
Zlobin S.K., Michnev M.M., Laptenok V.D., Bocharov A.N., Dolgopolov B.B.
ASSESSMENT OF SPACECRAFT SOLAR ARRAY RELIABILITY DURING GROUND EXPERIMENTAL DEVELOPMENT TEST
Zakharov S.A.
1 - 19 of 19 Items

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