Pesquisa

INVESTIGATION OF CHARGE-DISCHARGE PROCESSES IN THE SPACECRAFT DETACHABLE CONNECTOR

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

(Rus)

Volume 17, Nº 3 (2016)

GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD

Yakovlev A., Vnukov A., Balandina T., Balandin E., Tarletskiy I.

Volume 24, Nº 3 (2023)

Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit

Koroleva Y., Hohlov A., Nikolaev D., Borisova N., Mathynenko M.

(Rus)

(Eng)

Volume 24, Nº 2 (2023)

Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit

Koroleva Y., Hohlov A., Nikolaev D., Borisova N., Mathynenko M.

(Rus)

Volume 24, Nº 3 (2023)

The method of Haar sums for numerical solution of kinematic Poisson equations system that determine an evolution of a spacecraft position

Kirillov K., Ovchinnikova E., Safonov K., Titov G., Khokhlov A., Gashin A.

(Rus)

(Eng)

Volume 25, Nº 1 (2024)

Study of the payload extraction trajectory heavy class carrier rocket

Bordachev V., Kolga V.

(Rus)

(Eng)

Volume 21, Nº 2 (2020)

Inter-satellite optical communication link

Aleksandrov A., Vasilenko A., Korolev D.

(Eng)

Volume 21, Nº 4 (2020)

On remote sensing of the earth by spacecraft

Shlepkin A., Shiryaeva T., Shlepkin A., Filippov K., Pashkovskaya O.

(Eng)

Volume 22, Nº 1 (2021)

Multiversion model of software control systems for space vehicles with range of decision-making

Kartsan I., Efremova S.

(Rus)

(Eng)

Volume 24, Nº 2 (2023)

Development concept of inter-satellite laser communication

Kartsan I.

(Rus)

Volume 11, Nº 1 (2010)

The influence of conditions for passing GLONASSand GPS satellite radio navigation signals on the errors of defining relative coordinates

Garin E.

(Rus)

Volume 10, Nº 1-1 (2009)

The problems of telemetric data processingin the loop of spacecrafts computer-aided control system

Pakman D., Nekrasov M., Antamoshkin A.

(Rus)

Volume 12, Nº 2 (2011)

Dual-use spacecraft conception

Kislitskiy M., Kislitsky M.

(Rus)

Volume 10, Nº 2 (2009)

MA THEMA TICHAL PROVIDING OF THE PLANNING METHODOF SUPERVISORY EQUIPMENT SYSTEM PREP ARA TION FOR ELECTRONICAND RADIOTESTING OF SPACECRAFTS

Voronkovich V., Iosifov P.

(Rus)

Volume 15, Nº 1 (2014)

Automated control system of heat fluxes at thermovacuum testing of spacecrafts

Shevlyakov A., Vykhristyuk I., Verkhoglyad A., Khalimanovich V., Hristich V.

(Rus)

Volume 15, Nº 4 (2014)

Backgrounds and trends of all-electric propulsion geostationary satellites creation

Vnukov A., Rvacheva E.

(Rus)

ELASTIC FEED SYSTEMS OF FUEL TANKS

Platov I.

(Rus)

Volume 14, Nº 1 (2013)

Dynamical workbench for signature analysis and operating conditions of flywheel engine group of pointing and attitude control systems of spacecrafts

Synitskiy D., Murygin A.

(Rus)

MINIATURE ANTENNAS FOR CUBERSAT

Generalov A., Gadzhiev E.

(Rus)

IMPROVEMENT OF INSULATION RESISTANCE MEASUREMENT ACCURACY DURING SPACECRAFT POWER SYSTEM TESTS

Shtabel N., Samotik L., Mizrah E.

(Rus)

TO GEOSTATIONARY COLLOCATION PROBLEM

Kuprin A., Medvedev A.

(Rus)

Volume 17, Nº 4 (2016)

SOFTWARE SUPPORT FOR TESTING COMMAND RECEPTION AND TRANSMISSION AND TELEMETRY ANALYSIS IN THE COMMAND-AND-MEASURING SYSTEM

Nozhenkova L., Isaeva O., Vogorovskiy R., Gruzenko E.

Volume 16, Nº 1 (2015)

FEATURES OF DEVELOPMENT OF THE COMBINED IMPELLENT INSTALLATION AND THE CIRCUIT OF FLIGHT OF THE SPACECRAFT «INTERGELIO-PROBE»

Platov I., Simonov A., Konstantinov M.

(Rus)

Volume 25, Nº 1 (2024)

Calculation of the coupling loss factors for the angle connected beams

Kravchunovky A.

(Rus)

(Eng)

Volume 21, Nº 2 (2020)

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

Lomaev Y., Ivanov I., Tolstykh A., Islentev E.

(Eng)

Volume 21, Nº 3 (2020)

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

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

(Eng)

Volume 23, Nº 2 (2022)

Pressure measurement inside non-sealed equipment bay of the geostationary spacecraft

Mordovskiy S., Maximov I., Ivanov V., Sitnikova N., Trofimchuk D.

(Rus)

Volume 12, Nº 3 (2011)

ADAPTIVE MULTI BEAM ANTENNA JSC «ISS»

Pershin A., Uzolin E., Pershin A., Uzolin E.

(Rus)

Volume 10, Nº 5 (2009)

Geo satellite attitude and orbit control: fixed orbit control thrasters

Ermoshkin Y., Raevsky V., Urusov V.

(Rus)

Volume 13, Nº 2 (2012)

METHODS FOR HIGH-ACCURACY MEASUREMENTS OF PRECISION STRUCTURES FOR MOBILE AUTOMATIC SPACECRAFT IN THERMAL VACUUM CONDITIONS

Dvirniy G.

(Rus)

Volume 12, Nº 2 (2011)

Electric propulsions rational application range on the applied spacecrafts

Ermoshkin Y., Yermoshkin Y.

(Rus)

Volume 11, Nº 2 (2010)

MODERN SPACECRAFTS OPERATIONAL RELIABILITY AND QUALITY ANALYSIS

Patraev V., Trifanov I., Patraev V., Trifanov I.

(Rus)

Volume 15, Nº 1 (2014)

Rational photovoltaic batteries mounting on the earth remote sensing microsatellite

Gubin S., Shepetov Y., Dolzhukova K.

(Rus)

Volume 15, Nº 2 (2014)

Mathematical methods used to assess the position and form accuracy of a large-sized spacecraft reflector

Goldobin N.

(Rus)

PROBLEMS OF DEVELOPMENT OF LOW-ORBIT MULTIFUNCTIONAL PERSONAL SATELLITE COMMUNICATION SYSTEM «GONETS-D1M»

Kuzovnikov A., Testoedov N., Agureev V.

(Rus)

ONBOARD COMPUTER COMPLEX FOR UNPRESSURISED LONG-RESOURCED SPACECRAFTS

Kozlov I.

(Rus)

THE REVIEW OF MODERN SOLAR CELLS FOR SPACE APPLICATION BASED ON AIIIBV MATERIALS

Slyshchenko E., Naumova A., Lebedev A., Genali M., Vagapova N., Zhalnin B.

(Rus)

Volume 19, Nº 1 (2018)

ANALYSIS OF SPACECRAFT ORBITAL MOTION STABILITY OF GONETS-M NO 37152

Kolovsky I., Shmakov D., Podolyakin V.

(Rus)

Volume 18, Nº 1 (2017)

THE EVOLUTION OF THE PROJECT “SEA LAUNCH” OF SPACECRAFT

Testoedov N., Dvirnyi V., Krushenko G., Dvirnyi G.

(Rus)

Volume 18, Nº 1 (2017)

DETERMINATION OF THE FUNDAMENTAL FREQUENCY OF A SANDWICH PANEL AS CONSTRUCTIONAL PART OF SPACECRAFT BODY

Deev P., Sinkovskiy F.

(Rus)

Volume 17, Nº 2 (2016)

APPLICATION OF THE METHOD OF LOAD TESTING WITH GROUND experimental METHOD of CONTROL UNITS OF antenna GUIDANCE system

Kudryashova G., Babanov D., Galimzyanov A.

Volume 16, Nº 1 (2015)

The shock-absorber for executive powers of system of stabilisation of a spaceCRAFT

Vasiltsov A., Lipovtsev A.

(Rus)

Volume 24, Nº 3 (2023)

Ensuring the thermal regime of spacecraft structures

Shatrov A., Rabetskaya O., Fisenko E.

(Rus)

(Eng)

Volume 20, Nº 4 (2019)

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

Aliseenko Y., Nesterishin M., Vorontsova E., Fedosov V., Panteleev V.

(Eng)

Volume 21, Nº 3 (2020)

Development of the heat panel of the small space apparatus for navigation support

Kolga V., Yarkov I., Yarkova E.

(Eng)

Volume 23, Nº 2 (2022)

Small satellites for sea surface sounding

Kartsan I., Zhukov A.

(Rus)

Volume 11, Nº 6 (2010)

SOLAR BATTERIES EXPERIMENTALUNIT WITH CONCENTRATOR:IDEA, CONSTRUCTION, METHODOLOGY OF FLIGHT TESTS

Mel'nikov P., Kudryashov V., Kuzoro V., Shangina E., Melnikov P., Kudryashov V., Kuzoro V., Shangina E.

(Rus)

Volume 10, Nº 4 (2009)

GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS

Yermoshkin Y., Raevsky V., Urusov V.

(Rus)

Volume 13, Nº 5 (2012)

METHODOLOGICAL BASES OF ESTIMATION OF SYSTEMIC ACTION OF ADDITIONAL PAYLOAD ON SPACECRAFT FUNCTIONING

Kislitskiy M.

(Rus)

Volume 12, Nº 1 (2011)

CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT

Ermoshkin Y., Urusov V., Yermoshkin Y., Urusov V.

(Rus)

Volume 11, Nº 4 (2010)

GEOSTATIONARY SPACECRAFT ORBIT SLAVING AND MANEUVER: THRUSTERS ON DRIVES INSTALLATION SCHEME

Ermoshkin Y., Raevskiy V., Urusov V., Yermoshkin Y., Raevsky V., Urusov V.

(Rus)

Volume 15, Nº 4 (2014)

Mobile system weightlessness simulation for a large spacecraft

Kovalev I., Kikot J.

(Rus)

Volume 15, Nº 1 (2014)

Unification methods of present telemetry processing systems in satellite control centers

Nekrasov M., Packman D., Antamoshkin A.

(Rus)

MICROELECTRONIC SYSTEMS FOR AUTOMATION OF PERSPECTIVE SPACE VEHICLES

Nepomnuashy O., Ohotkin K., Habarov V.

(Rus)

DEVELOPMENT OF COMPOSITE PRECISION SATELLITE REFLECTOR: FINITE ELEMENT CONSTRUCTION MODELING

Lopatin A., Pasechnik K., Vlasov A., Shatov A.

(Rus)

Volume 19, Nº 3 (2018)

ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT

Yermoshkin Y., Volkov D., Yakimov E.

(Rus)

THE METHOD OF AUTOMATED DEVELOPMENT OF AN ASSEMBLY DRAWING OF A CABLE NETWORK

Butin A., Dubrovskiy E., Dobyshev E., Efremov S., Suntsov S.

(Rus)

SIMULATION MEANS OF ELECTROSTATIC DISCHARGES IN THE SYSTEM “STATIONARY PLASMA THRUSTER - TRANSFORMATION AND CONTROL SYSTEM”

Trofimchuk D., Bezhayev Y., Ivanov V., Kochura S., Maximov I.

(Rus)

Volume 17, Nº 3 (2016)

FREQUENCY ANALYSIS OF THE LONGITUDINAL AND TRANSVERSE VIBRATIONS OF LATTICE CYLINDRICAL SHELL WITH OPENINGS

Shatov A., Khakhlenkova A.

Volume 16, Nº 1 (2015)

AN ELECTROMECHANICAL EXECUTIVE BODY BASED ON THE CONTACTLESS DIRECT CURRENT MOTOR WITH A WINDING PRINTING DISK STATOR FOR SMALL SPACECRAFTS

Balandina T., Balandin E.

(Rus)

Volume 20, Nº 3 (2019)

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

Platov I., Simonov A., Vorobyev A., Gordienko E.

(Eng)

Volume 22, Nº 4 (2021)

Alternative method of solar simulation for thermal vacuum tests of spacecraft

Shevchuk A.

(Rus)

(Eng)

Volume 23, Nº 1 (2022)

Methodological principles of space vehicle design for the maximum energy sup-ply of the payload

Chebotarev V., Fatkulin R., Vorontsova E., Balandina T., Shangina E.

(Rus)

Volume 24, Nº 1 (2023)

Design of a thermal control system with a two-phase coolant for a spacecraft with a capacity of 7 kW

Shilkin O., Kolesnikov A., Delkov A., Kishkin A., Shevchenko Y.

(Rus)

Volume 10, Nº 5 (2009)

Development of mechanical test procedure for the fuel bellows tanks

Ermoshkin Y., Orlov S., Usanov A.

(Rus)

Volume 13, Nº 5 (2012)

DEVELOPMENT AND THERMAL VACUUM TESTS OF HEAT SHIELDS FOR PROTECTION OF MECHANICAL ELECTRIC DRIVE UNIT FROM EFFECT OF “SOLAR TRAP”

Vshivkov A., Tanasienko F., Golovenkin E., Yurtaev E.

(Rus)

Volume 12, Nº 1 (2011)

UPGRADING OF PHOTOVOLTAICARRAY SIMULATORWITH TWO-CIRCUIT CONTROL ELEMENT

Tkachev S., Mizrakh E., Tkachev S., Mizrakh E.

(Rus)

Volume 16, Nº 2 (2015)

TOP-DOWN APPROACH FOR SPACECRAFT DEVELOPMENT

Lihachev M.

(Rus)

Volume 15, Nº 2 (2014)

Designing and constructing of the program-mathematical model for the spacecraft command and measuring system

Nozhenkova L., Isaeva O., Gruzenko E.

(Rus)

Volume 15, Nº 4 (2014)

The research of effective thermal conductivity coefficient effect on the temperature field of reflector

Burova O., Romankov E., Tsivilev I., Minakov A.

(Rus)

SEPARATION DEVICE FOR SPACECRAFT UNPRESSURIZED PLATFORMS BASED ON ISOGRID STRUCTURES

Vehov A.

(Rus)

PROGRAM COMPLEX FOR MODELING OF STABILIZED MOTION OF SPACECRAFT WITH TRANSFORMABLE FLEXIBLE PARTS

Ignatyev M., Kopylov V., Kulakov A., Sotnikov M.

(Rus)

MATHEMATICAL MODEL FOR GEOSTATIONARY SPACECRAFT DISTURBING TORQUES DETERMINATION

Latyntsev S., Murygin A.

(Rus)

Volume 19, Nº 3 (2018)

TWO-DIMENSIONAL THERMAL MODEL OF THE THERMAL CONTROL SYSTEM FOR NONHERMETIC FORMATION SPACECRAFT

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

(Rus)

Volume 18, Nº 1 (2017)

SOFTWARE SUPPORT FOR TESTING of large spacecraft REFLECTOR AND EVALUATION OF THE OPERATION PARAMETERS OF COMPONENT WEIGHT COMPENSATION SYSTEM

Kovalev I., Badanina J.

(Rus)

Volume 17, Nº 3 (2016)

DOUBLE-CONIC ADAPTER FOR LAUNCHING THE BLOCK OF THREE SPACECRAFTS

Khakhlenkova A.

Volume 17, Nº 4 (2016)

ASSESSMENT OF SPACECRAFT SOLAR ARRAY RELIABILITY DURING GROUND EXPERIMENTAL DEVELOPMENT TEST

Zakharov S.

Volume 16, Nº 3 (2015)

REDUCTION OF SPACECRAFT HARNESS MASS

Dvirnyi V., Eremenko N., Dvirnyi G.

Volume 25, Nº 3 (2024)

Innovative technical solutions developed under the leadership of M. F. Reshetnev in the creation of the first Siberian launcher “Cosmos-3M”

Nazarov V., Golovenkin E., Piunov V.

(Rus)

(Eng)

Volume 20, Nº 2 (2019)

Control and regulation equipment of electric power system for a prospective piloted transport system

Savenkov V., Tishchenko A., Volokitin V.

(Eng)

Volume 22, Nº 4 (2021)

Development of workspace and algorithms for testing SpaceWire onboard equipment

Maksyutin A., Murygin A., Ivlenkov D., Dymov D.

(Rus)

(Eng)

Volume 23, Nº 4 (2022)

Testing of spacecraft orientation and stabilization systems sing starry sky simulators

Gorelko M., Murygin A.

(Rus)

Volume 24, Nº 1 (2023)

Development of the CYCLOPS CubeSat payload

Sotnikova N., Kadadova A., Utkin V., Kadochnikov D.

(Rus)

Volume 10, Nº 5 (2009)

Implementation error of relative measurements

Garin E.

(Rus)

Volume 24, Nº 1 (2023)

Ground control system for distant space vehicles

Zhukov A., Ivanov K., Bondareva M., Bondarev M., Gorovoy D.

(Rus)

Volume 11, Nº 7 (2010)

THE INFLUENCE OF CONDITIONS FOR PASSING GLONASS AND GPS SATELLITE RADIO NAVIGATION SIGNALS ON THE ERRORS OF DEFINING RELATIVE COORDINATES

Garin E.

(Rus)

Volume 17, Nº 1 (2016)

PLATFORM OF AUTOMATION OF COMPONENT WEIGHT COMPENSATION SYSTEM FOR LARGE SPACECRAFT REFLECTOR

Kovalev I., Badanina J.

Volume 15, Nº 5 (2014)

Review of technical solutions for developing of a control and data handling as a system on a chip for ultra small spacecraft

Khanov V., Borodina T., Antamoshkin A.

(Rus)

Volume 14, Nº 5 (2013)

SOME RESULTS OF “PLASMA-PROGRESS” AND “RADAR-PROGRESS” ACTIVE SPACE EXPERIMENTS

Khakhinov V., Potekhin A., Lebedev V., Kushnarev D., Alsatkin S.

(Rus)

DEPLOYMENT DYNAMICS MATHEMATICAL MODELS USED FOR THE OVERSIZED TRANSFORMABLE MECHANICAL SYSTEMS DURING ON-GROUND COMPLEX FUNCTIONAL TESTS

Romanenko I., Dvirnyy V., Kuklin V., Perminov M.

(Rus)

Volume 14, Nº 2 (2013)

SIMULATION MODELING OF THE MAIN COMPONENTS OF MOTION CONTROL SYSTEM OF THE SATELLITE

Yelubayev S., Jamalov N., Alipbayev K., Sukhenko A., Bopeyev T.

(Rus)

Volume 19, Nº 4 (2018)

METHOD FOR CALCULATING THE ENERGY CHARACTERISTICS AND SOLAR BATTERY PARAMETERS OF HIGH-VOLTAGE POWER SUPPLY SYSTEMS

Chernaya M.

(Rus)

Volume 19, Nº 1 (2018)

VERIFICATION OF FINITE-ELEMENT MODEL SPACECRAFT VIA TEST RESULTS

Balyakov D.

(Rus)