Научные статьи \ Прикладные науки. Медицина. Технология \ Инженерное дело. Техника в целом

Техника средств транспорта - 629

Научные статьи

В разделе "Техника средств транспорта"
Наведение и управление космическим роботом при перелетах в низкоорбитальной группировке мини-спутников землеобзора
Имитация и анимация в среде Sirius-S для проектирования и поддержки систем управления космических аппаратов
Наведение и управление ориентацией спутника при отказах в кластере реактивных маховиков
Адаптивно-управляемый метод мониторинга экологических параметров беспилотных транспортных средств
Обеспечение долговечности и надежности контактных колец токосъемных устройств при работе в упруго-пластическом состоянии
Использование принципа гравитационной стабилизации и ориентации при проектировании малых космических аппаратов
Уточнение границ зоны пластических деформаций диафрагмы топливного бака
Исследование параметров движения входа космоплана в атмосферу
Development of workspace and algorithms for testing SpaceWire onboard equipment
Development of a model for detecting malfunctions during the maintenance of aircraft units and systems
Alternative method of solar simulation for thermal vacuum tests of spacecraft
Methodological principles of space vehicle design for the maximum energy supply of the payload
Development of a methodology for testing SpaceWire network switches
Pressure measurement inside non-sealed equipment bay of the geostationary spacecraft
The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine
Design of the fastening assembly of the guys on the power spokes reflector
The concept of an educational and scientific experiment for conducting on-orbit testing of any types of photovoltaic cell
Methodological principles for the formation of a number of unified space communication satellite platforms
On the issue of hydrodynamic braking efficiency dur-ing high-velocity tests on a rocket-rail track
Increasing the specific impulse of an oxygen-hydrogen liquid rocket engine by in-creasing heat transfer in the combustion chamber
Testing of spacecraft orientation and stabilization systems using starry sky simulators
Specialized LED assembly for out-atmospheric solar simulator
Experimental determination of vibration conductivity by rocket sled structural elements in high-speed track tests of aircraft equipment
Studying static stability of a model rocket
Ground control system for distant space vehicle
The main provisions of the methodology for ensuring the resistance of the onboard equipment of spacecraft to the effects of the radiation effects of outer space
The aircraft hydraulic system units and pipelines heat exchange parameters study
Development of the CYCLOPS CubeSat payload
Parametric analysis of the strength of a solid propellant rocket engine nozzle
Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit
Ensuring the thermal regime of spacecraft structures
Evaluation of the main parameters of ReshUCube-1 telemetry over a period of 10 months in orbit
Calculation of the parameters and characteristics of a rotating lunar jet penetrator
Features of reaching limiting speed values of track tests of ballistic type aircraft
Verification of thermodynamic parameters of a mixture of generator gas on oxygen-hydrogen fuel with an excess of one of the fuel components
Study of the payload extraction trajectory heavy class carrier rocket
Ensuring durability and reliability of contact rings of current collection devices when working in elastic-plastic state
Research of the motion parameters of a spaceplane entry of into the atmosphere
Innovative technical solutions developed under the leadership of M. F. Reshetnev in the creation of the first Siberian launcher “Cosmos-3M”
Increasing the capabilities of a test ballistic missile to separate test objects
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