Страница 75. Техника средств транспорта УДК: 629

Авиационная промышленность России: современные проблемы и перспективы развития

Кузьмина Людмила Викторовна

Анализ и группировка проблем развития многотопливных автозаправочных станций в России

Тавдидишвили Александр Евгеньевич, Зинин Василий Леонидович, Тихонова Майя Владимировна

Моделирование параметров технического состояния стартерных аккумуляторных батарей

Пузаков Андрей Владимирович, Калимуллин Руслан Флюрович, Смирнов Дмитрий Андреевич

Выявление зависимости показателя давления в тормозной системе от величины износа уплотнительных манжет как способ диагностирования ресурсного состояния гтц автомобиля

Кобозев Сергей Васильевич, Баженов Юрий Васильевич

Estimation of the efficiency of spacecraft transportation with minimal radiation degradation of solar cells

Birukov V. I., Nazarov V. P., Kurguzov A. V.

An approach to ground testing of rockets and space vehicles on transient processes by copra-spring stand

Bondarenko A. Yu, Mitin A. Yu., Tolchenov V. A., Eykhorn A. N., Yuranev O. A.

Parametric identification of the heat condition of radio electronic equipment in airplane compartment

Gusev S. A., Nikolaev V. N.

The definite questions of simulation of transformable space structures dynamics

Zhang Zikun, Zimin V. N., Krylov A. V., Churilin S. A.

Applying software-mathematical models of onboard equipment to develop onboard software

Lomaev Yu. S., Ivanov I. A., Tolstykh A. V., Islentev E. V.

Developing the laboratory test bench of fuel three-point measurement

Akzigitov R. A., Pisarev N. S., Statsenko N. I., Glukharev A. R., Tsar’kov I. B.

Solar thermal propulsion systems with various high-temperature power sources

Finogenov S. L., Kolomentsev A. I.

Real-time carrier rocket mission control using space relay system

D. A. Makhalov, M. P. Nikitina, S. B. Usikov, A. V. Manoilo

Development of the propulsion construction and the trajectory of the spacecrafts for the study of Martian planetary system

I. V. Platov, A. V. Simonov, A. L. Vorobyev, E. S. Gordienko

Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system

Yu. N. Shevchenko, A. A. Kishkin, F. V. Tanasiyenko, O. V. Shilkin, M. M. Popugayev

Calculation of complex heat transfer in the liquid circuit of the spacecraft thermal control system based on real topology and thermophysical properties

Yu. N. Shevchenko, A. A. Kishkin, F. V. Tanasiyenko, O. V. Shilkin, S. N. Sokolov

Additional screening tests at the testing technical center for ground power equipment

Aliseenko Y. V., Nesterishin M. V., Vorontsova E. O., Fedosov V. V., Pateleev V. I.

Spacecraft motion in a low circular orbit in establishing intersatellite link

Kolovsky I. K., Shmakov D. N.

Analysis of the ADS-B airspace monitoring system

Akzigitov A. R., Akzigitov R. A., Ogorodnikova U. V., Dmitriev D. V., Andronov A. S.

To the question of forecasting the technical condition of low-thrust liquid rocket engines

Komlev G. V., Mitrofanova A. S.

Peculiar properties of technological improvement and optimization of production costs of 3D-configuration pipes

Titenkov S. V., Zhuravlev V. Yu.

Remotely operated underwater vehicle in the form of a quadcopter: features of the design and control system

D. A. Volkov, A. V. Sayapin, K. V. Safonov, A. A. Kuznetsov

Study of impeller design parameters effect on the axial thrust of a centrifugal electric pump assembly

Z. A. Kuznetsova, M. I. Sinichenko, A. D. Kuznetsov, I. A. Kleshnina, F. K. Sin'kovskiy

Influence of plasma jets of electric jet engines on spacecraft functional characteristics

A. B. Nadiradze, S. G. Kochura, I. A. Maximov, R. E. Tikhomirov, S. V. Balashov

Development of the concept of a reusable liquid rocket engine with three-component fuel

Belyakov V. A., Vasilevsky D. O., Ermashkevich A. A., Kolomentsev A. I., Farizanov I. R.

Experimental investigations of a plasma thrusters and its power processing units performances like an electric load of a spacecraft’s power condition system

Ermoshkin Yu. M., Kochev Yu. V., Nikihelov A. V., Pervukhin A. V., Simanov R. S.

Engeneering of a cooling system for a reusable liquid-propellant rocket engine opereting on tripropellant fuel

Belyakov V. A., Vasilevsky D. O., Ermashkevich A. A., Kolomentsev A. I., Farizanov I. R.

Optimization the position of the spacecraft instrument panel mounting points based on modal analysis

Kolga V. V., Lykum A. I., Marchuk M. E., Filipson G. U.

Characteristics of low thrust liquid-propellant rocket engines testing process

Nazarov V. P., Piunov V. Yu., Yatsunenko V. G., Savchin D. A.

Дистанционно-управляемый подводный аппарат в форме квадрокоптера: особенности конструкции и системы управления

Волков Д.А., Саяпин А.В., Сафонов К.В., Кузнецов А.А.

Modeling of spectroerergetic characteristics of space objects in the optical range

Bogoyavlenskiy A.I., Kamenev A.A., Poluyan M.M., Soluyanov A.A.

Вычислительный эксперимент по получению характеристик моделируемой системы терморегулирования космического аппарата

Танасиенко Ф.В., Шевченко Ю.Н., Делков А.В., Кишкин А.А., Мелкозеров М.Г.

Development of three-point aviation fuel quantity gauge

Akzigitov R.A., Statsenko N.I., Pisarev N.S., Efimova A.N.

The method of automated development of an assembly drawing of a cable network

Butin A.M., Dubrovskiy E.U., Dobyshev E.V., Efremov S.V., Suntsov S.B.

Mathematical model for geostationary spacecraft disturbing torques determination

Latyntsev S.V., Murygin A.V.

Investigation of charge-discharge processes in the spacecraft detachable connector

Tikhomirov R.E., Maximov I.A., Trofimchuk D.A., Ivanov V.V., Balashov S.V.

Analysis of microstructure of laminated polymer composite material of metal composite overwrapped pressure vessel

Eremin N.V.

Two-dimensional thermal model of the thermal control system for nonhermetic formation spacecraft

Tanasienko F.V., Shevchenko Y.N., Delkov A.V., Kishkin A.A.

Application of the bootstrap method for statistical characteristics assessment of aircraft components’ small samples

Gerasimova D.S., Sayapin A.V., Palukhin A.A., Katsura A.V.

On the concept of all electric propulsion spacecraft

Yermoshkin Yu. M., Volkov D.V., Yakimov E.N.

Разработка двигательной установки на базе двигателей малой тяги и схемы полёта космических аппаратов к центру солнечной системы

Платов И.В., Симонов А.В.

Техника средств транспорта - 629

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