Transport vehicle engineering - 629

Scientific articles

In section "Transport vehicle engineering"
Feasibility analysis of liquid propellant settling in the tanks of a space propulsion system after flying in zero gravity using a separating turn maneuver of the orbital unit
Tupitsyn Nikolay Nikolaevich
Results of studies of the processes of clearing of gaseous contaminants and ventilating the atmosphere of habitable pressurized modules in a space station
Elchin Anatoly Petrovich, Guzenberg Arkady Samuilovich, Romanov Sergey Yurievich, Zheleznyakov Aleksandr Grigorievich, Ryabkin Aleksandr Moiseevich
Chronicle of an extraordinary space journey (ballistic analysis of Soyuz T-15 flight)
Soloviev V.A., Murtazin R.F., Melnikov E.K.
Combining heritage and spirit of innovation
Karchaev Kh.zh., Primakov P.V., Galich N.V.
Spacecraft rendezvous and docking using measurements from satellite navigation equipment combined with the optical subsystem for final approach
Orlovskiy I.V., Mikhailov M.V., Rozhkov S.N., Avanesov G.A., Zhukov B.S.
Contamination levels measuring in external induced atmosphere of Russian orbital stations and the Russian segment of the International Space Station
Dushin V.K., Krylov A.N., Skorovarov A.Yu.
Methods and results of extending the life of the International Space Station Russian segment
Milovanov Viktor Aleksandrovich, Agafonov Mikhail Mikhailovich, Filippov Ilya Mikhailovich
Specificities of landing propulsion system jets’ gas dynamic effects on re-entry vehicle and ground surface during landing
Pavlov Aleksandr Olegovich, Simakova Tatiana Vladimirovna
Trajectory options for a manned mission to mars using high-thrust propulsion systems
Arkhangelskiy Nikolay Ivanovich, Muzychenko Evgeny Igorevich, Sinitsin Aleksey Andreevich
A method of using fuzzy hypergraphs to evaluate structural and technological survivability of attitude control systems for unmanned spacecraft
Pavlov Aleksandr Nikolaevich, Pavlov Dmitry Aleksandrovich, Vorotyagin Valentin Nikolaevich
Integration of controllable scientific equipment into the Russian segment of the international space station
Ayukaeva Diana Maratovna, Voronin Fedor Andreevich, Poluarshinov Mikhail Andreevich, Kharchikov Mikhail Aleksandrovich
A review of high-power magnetoplasmodynamic electric propulsion designs and studies of RSC Energia
Sinyavskiy Victor Vasilievich
Main design characteristics of small scientific and applied-purpose spacecraft based on the AIST-2 unified platform
Kirilin Aleksandr Nikolaevich, Akhmetov Ravil Nurgalievich, Baklanov Aleksandr Ivanovich, Stratilatov Nikolay Remirovich, Abrashkin Valeriy Ivanovich, Kosmodemyansky Evgeniy Vladimirovich, Tkachenko Sergey Ivanovich, Salmin Vadim Viktorovich, Tkachenko Ivan Sergeevich, Safronov Sergey Lvovich
Experimental development onboard the ISS Russian segment of the prototype system for quick localization of a puncture in the space station pressure shell
Markov Aleksandr Viktorovich, Konoshenko Viktor Petrovich, Churilo Igor Vladimirovich, Churilo Oleg Vladimirovich, Sokolov Vyacheslav Georgievich, Gorbenko Andrey Vladimirovich, Buslov Evgeniy Pavlovich, Ustinov Vladimir Vasilyevich, Feldstein Valeriy Adolfovich, Skalkin Aleksandr Sergeevich
Small spacecraft-based space system for real-time earth surface monitoring
Danilkin Aleksandr Petrovich, Voronkov Vladimir Nikolaevich, Kazantsev Oleg Yuryevich, Ketov Vyacheslav Aleksandrovich, Koptev Yury Nikolayevich, Plastinin Yury Aleksandrovich, Strulya Igor Leonardovich, Tatarnikov Aleksandr Vladimirovich
On attached masses of panels oscillating in incompressible medium
Buzhinskiy Valery Alekseevich
On the development of testing facilities for the scientific testing center of the rocket and space industry for developmental testing of advanced cryogenic propulsion systems
Sizyakov Nikolay Petrovich, Yuriev Igor Anatolievich, Galeev Ayvengo Gadyevich
Conceptual scenarios for development of ground infrastructure for receiving mission payload data from a perspective Earth remote sensing satellite constellation
Ereshko M.V., Borisov A.V.
The small spacecraft with a magnetic sail on high-temperature superconductors
Kombaev T.Sh., Artemov M.E., Sysoev V.K., Dezhin D.S.
On the feasibility of developing a single-stage acceleration/deceleration unit based on the oxygen-hydrocarbon engine 11D58M for a super-heavy launch vehicle
Sokolov B.A., Tupitsyn N.N., Tumanin E.N., Kryukov I.A., Kiselev A.V., Firstaev D.S.
Conceptual design studies of an electrically propelled upper stage for deployment of a multi-plane orbital constellation of small spacecraft
Levandovich A.V., Mosin D.A., Sinyavskiy V.V., Tyutyukin A.E., Urtmintsev I.A.
Developing methods for taking into account the radiation coming from earth in simulations of incoming electric power on the Russian segment of the International Space Station in experiment Albedo
Rulev Dmitry Nikolaevich
A review of exploratory studies at RSC Energia into high-temperature voltage conversion systems for an electrically-propelled transportation spacecraft
Sinyavskiy Viktor Vasilyevich, Troitskiy Stanislav Rafailovich
Pressure measurement of induced external atmosphere on the Russian segment of the International Space Station in experiment "Control"
Aleksandrov Eduard Nikolaevich, Antipova Maya Stanislavovna, Kashkovskiy Aleksandr Vladimirovich, Krylov Andrey Nikolaevich, Rodicheva Anna Alekseevna
Moscow international symposia on solar system research (10M-S3 and 11M-S3) reports review. Part 1. Mars exploration
Evdokimov Roman Aleksandrovich
The computer method for choosing the parameters of the peripheral docking unit's latch mechanism
Chernyshev Ivan Evgenyevich
Spacecraft reliability calculations using statistical regularities in occurrences of failures in devices, units and assemblies during their operation
Milovanov Viktor Aleksandrovich
Use of methane in closed-loop life support systems for space missions
Zheleznyakov Alexandr Grigorievich, Glukhikh Sergey Aleksandrovich, Guzenberg Arkady Samuilovich, Romanov Sergey Yurievich, Yurgin Aleksey Viktorovich, Ryabkin Aleksandr Moiseevich
Past experience and future prospects for launching our country's small spacecraft from Plesetsk launch site
Bashlyaev Nikolay Andreevich, Nikolaev Aleksey Yurievich, Duga Vadim Vadimovich, Mosin Dmitry Aleksandrovich
An analytical method for the dynamic response prediction and produced test modes generated by vibro-shock test benches
Komarov Ilya Sergeevich, Feldshteyn Valery Adolfovich
Automated monitoring of flatness of solar array wings
Marinin Vladimir Ivanovich, Zhurikhin Sergey Mikhaylovich, Kireev Denis Mikhaylovich, Andreev Dmitry Stanislavovich, Andreeva Natalya Olegovna, Kopyl Nikolay Ivanovich, Senkovskiy Aleksandr Nikolaevich, Ilyushenkov Sergey Frolovich, Churkin Sergey Nikolaevich
Method for calculating the duration of communication sessions with a spacecraft under constraints of the communications coverage of the command and tracking station
Zhigastova Olga Konstantinovna, Smolokovskiy Andrey Valeryevich, Usikov Sergey Borisovich
On complexity-level based classification of regenerative life support systems for manned spacecraft
Potemkin Artur Lvovich, Glebov Igor Vasilievich
Using led lamps in simulators of the Russian segment modules of the International Space Station
Batrakov Valery Vitalyevich, Spirin Andrey Evgenyevich, Atroshchenko Vladimir Ilyich, Kutina Irina Vladimirovna
Alternating current power generating system for closed-loop gas-turbine system of a spacecraft
Gotovtsev Kirill Vladimirovich, Koshlakov Vladimir Vladimirovich, Oshev Yury Arkadyevich
Procedures for cognitive and synergetic observation and proactive control of power capacity of nickel-hydrogen storage batteries onboard a geostationary spacecraft
Kovtun Vladimir Semenovich
Velocity and distribution velocity of meteoroids and space debris in near-earth space
Mironov Vadim Vsevolodovich, Tolkach Mikhail Aleksandrovich
Determining parameters of sandwich composite panels for Earth remote sensing satellite bus
Gorodetskiy Mikhail Alekseevich, Mikhailovskiy Konstantin Valerievich, Reznik Sergey Vasilyevich
Possible engineering design solutions for development of heavy and super-heavy oxygen-kerosene space rocket
Katorgin Boris Ivanovich, Lopota Vitaly Aleksandrovich, Levochkin Petr Sergeevich, Chvanov Vladimir Konstantinovich, Samitov Rashit Makhmutovich, Sokolov Boris Aleksandrovich, Filippov Ilya Mikhaylovich, Ulybyshev Yury Petrovich, Murtazin Rafail Farvazovich, Tupitsyn Nikolay Nikolaevich, Kryukov Igor Aleksandrovich, Kiselev Andrey Valeryevich, Firstaev Dmitry Sergeevich
A method for verifying the model of tank operational pressurization process during development of propellant supply system in liquid rocket engines of launch vehicle propulsion systems
Bershadskiy Vitaliy Aleksandrovich, Sokolov Boris Aleksandrovich, Tumanin Evgeny Nikolaevich