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Authors

Vol 22, No 4 (2021)

Alternative method of solar simulation for thermal vacuum tests of spacecraft

Shevchuk A.A.

(Rus)

(Eng)

Vol 23, No 1 (2022)

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

Chebotarev V.E., Fatkulin R.F., Vorontsova E.O., Balandina T.N., Shangina E.A.

(Rus)

Vol 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.V., Kolesnikov A.P., Delkov A.V., Kishkin A.A., Shevchenko Y.N.

(Rus)

Vol 10, No 5 (2009)

Development of mechanical test procedure for the fuel bellows tanks

Ermoshkin Y.M., Orlov S.A., Usanov A.Y.

(Rus)

Vol 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.Y., Tanasienko F.V., Golovenkin E.N., Yurtaev E.V.

(Rus)

Vol 12, No 1 (2011)

UPGRADING OF PHOTOVOLTAICARRAY SIMULATORWITH TWO-CIRCUIT CONTROL ELEMENT

Tkachev S.B., Mizrakh E.A., Tkachev S.B., Mizrakh E.A.

(Rus)

Vol 16, No 2 (2015)

TOP-DOWN APPROACH FOR SPACECRAFT DEVELOPMENT

Lihachev M.V.

(Rus)

Vol 15, No 2 (2014)

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

Nozhenkova L.F., Isaeva O.S., Gruzenko E.A.

(Rus)

Vol 15, No 4 (2014)

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

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

(Rus)

Vol 14, No 6 (2013)

SEPARATION DEVICE FOR SPACECRAFT UNPRESSURIZED PLATFORMS BASED ON ISOGRID STRUCTURES

Vehov A.S.

(Rus)

Vol 14, No 3 (2013)

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

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

(Rus)

Vol 19, No 2 (2018)

MATHEMATICAL MODEL FOR GEOSTATIONARY SPACECRAFT DISTURBING TORQUES DETERMINATION

Latyntsev S.V., Murygin A.V.

(Rus)

Vol 19, No 3 (2018)

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.

(Rus)

Vol 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.V., Badanina J.O.

(Rus)

Vol 17, No 3 (2016)

DOUBLE-CONIC ADAPTER FOR LAUNCHING THE BLOCK OF THREE SPACECRAFTS

Khakhlenkova A.A.

Vol 17, No 4 (2016)

ASSESSMENT OF SPACECRAFT SOLAR ARRAY RELIABILITY DURING GROUND EXPERIMENTAL DEVELOPMENT TEST

Zakharov S.A.

Vol 16, No 3 (2015)

REDUCTION OF SPACECRAFT HARNESS MASS

Dvirnyi V.V., Eremenko N.V., Dvirnyi G.V.

Vol 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.P., Golovenkin E.N., Piunov V.Y.

(Rus)

(Eng)

Vol 20, No 2 (2019)

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

Savenkov V.V., Tishchenko A.K., Volokitin V.N.

(Eng)

Vol 22, No 4 (2021)

Development of workspace and algorithms for testing SpaceWire onboard equipment

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

(Rus)

(Eng)

Vol 23, No 4 (2022)

Testing of spacecraft orientation and stabilization systems sing starry sky simulators

Gorelko M.G., Murygin A.V.

(Rus)

Vol 24, No 1 (2023)

Development of the CYCLOPS CubeSat payload

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

(Rus)

Vol 10, No 5 (2009)

Implementation error of relative measurements

Garin E.N.

(Rus)

Vol 24, No 1 (2023)

Ground control system for distant space vehicles

Zhukov A.O., Ivanov K.A., Bondareva M.K., Bondarev M.N., Gorovoy D.S.

(Rus)

Vol 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.N.

(Rus)

Vol 17, No 1 (2016)

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

Kovalev I.V., Badanina J.O.

Vol 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.K., Borodina T.V., Antamoshkin A.N.

(Rus)

Vol 14, No 5 (2013)

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

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

(Rus)

Vol 14, No 6 (2013)

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

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

(Rus)

Vol 14, No 2 (2013)

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

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

(Rus)

Vol 19, No 4 (2018)

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

Chernaya M.M.

(Rus)

Vol 19, No 1 (2018)

VERIFICATION OF FINITE-ELEMENT MODEL SPACECRAFT VIA TEST RESULTS

Balyakov D.F.

(Rus)

Vol 18, No 3 (2017)

STUDENT PICOSATELLITE PLATFORM SIBQUBE: DEVELOPMENT OF PROTOTYPE STRUCTURE OF POCKETQUB CLASS PICOSATELLITE

Kravchunovsky A.P., Draganyuk M.N., Zuev D.M., Skorobogatov S.A., Movchan P.V.

(Rus)

Vol 17, No 4 (2016)

LATTICE CYLINDRICAL SHELL WITH A ROUND TRANSVERSE PROFILE AND VARIABLE STIFFNESS

Khakhlenkova A.A.

Vol 17, No 2 (2016)

GEOMETRICAL AND FINITE-ELEMENT MODELING OF LATTICE CONICAL SHELL WITH GEODESIC PATH OF SPIRAL RIBS

Khakhlenkova A.A., Shatov A.V.

Vol 25, No 2 (2024)

Using the principle of gravitational stabilization and orientation in the design of small spacecraft

Еsina P.A., Kornev V.M.

(Rus)

Vol 20, No 2 (2019)

Development of interface module emulator architecture for spacecraft life support systems

Komarov V.A., Semkin P.V.

(Eng)

Vol 22, No 3 (2021)

Application of the propulsion subsystem on the base of SPT-100b plasmic thruster to the Express-80 and Express-103 spacecraft’s orbit raising and orbit control

Ermoshkin Y.M., Vnukov A.A., Volkov D.D., Kochev Y.V., Simanov R.S., Yakimov E.N., Grikhin G.S.

(Rus)

(Eng)

Vol 24, No 2 (2023)

Features of defining the damping function in spacecraft finite-element models

Kravchunovky A.P.

(Rus)

Vol 24, No 1 (2023)

Possibility of unification of requirements for radiation resistance for spacecraft with different operating conditions

Nazarenko A.A., Maximov I.A., Kochura S.G.

(Rus)

Vol 10, No 1-1 (2009)

The problems of the transform antennas manufacture and development

Dvirny G.V.

(Rus)

Vol 13, No 4 (2012)

TECHNIQUE FOR CALCULATION AND SELECTION OF SPACECRAFT ELECTRIC HEATERS PARAMETERS UNDER UNCERTAINTY CONDITIONS

Chebotarev V.E., Zvonar V.D., Fatkulin R.F., Dmitriev G.B.

(Rus)

Vol 10, No 2 (2009)

COMBINED METHOD OF GONETS-M SPACECRAFT CONTROL MUL TIVERSION SOFTW ARE DESIGN

Antamoshkin O.

(Rus)

Vol 17, No 1 (2016)

ADVANCED UNIFIED MICRO SERIES PLATFORMS

Zimin I.I., Valov M.V., Yakovlev A.V.

Vol 15, No 4 (2014)

Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts

Delkov A.V., Hodenkov A.A., Shevchenko Y.N.

(Rus)

Vol 14, No 3 (2013)

INVESTIGATION OF THE SPACE VEHICLES COATINGS FEATURES

Miheev A.E., Girn A.V., Ivasev S.S., Evkin I.V.

(Rus)

Vol 14, No 6 (2013)

SATELLITE MASS CRITERIA OPTIMIZATION WITH THE USE OF CAD “ACAB”

Kochev Y.V., Efremov S.V., Ovchinnikov A.V.

(Rus)

Vol 19, No 3 (2018)

PROCEDURE FOR EVALUATING THE EFFECTIVE USE RANGE OF THE UNIFIED SPACE PLATFORMS

Chebotarev V.E., Zimin I.I.

(Rus)

Vol 19, No 2 (2018)

ANALYSIS OF LED-BASED SOLAR SIMULATOR DEVELOPMENT CAPABILITY FOR SPACECRAFT GROUND TESTING APPLICATIONS

Dvirniy G.V., Shevchuk A.A., Dvirniy V.V., Elfimova M.V., Krushenko G.G.

(Rus)

Vol 18, No 4 (2017)

THE ALGORITHM FOR ESTIMATING ANGULAR RATE OF SPACECRAFT IN SURVIVABILITY MODE

Latyntsev S.V., Meus S.V., Оvсhinniкоv А.V.

(Rus)

Vol 18, No 3 (2017)

AUTOMATED WEIGHT COMPENSATION SYSTEM FOR GROUND-BASED TRYOUT OF SPACE VEHICLE SOLAR PANELS

Verhoglyad A.G., Kuklin V.A., Makarov S.N., Mihalkin V.M., Halimanovich V.I.

(Rus)

Vol 17, No 3 (2016)

DEVELOPMENT OF THE PROPULSION CONSTRUCTION AND THE TRAJECTORY FOR THE SPACECRAFTS OF THE “LAPLACE-L” MISSION FOR THE STUDY OF THE JUPITER PLANETARY SYSTEM

Platov I.V., Simonov A.V.

Vol 17, No 4 (2016)

THERMAL STORAGE TO THE TEMPERATURE CONTROL SYSTEM OF POWERFUL BLOCKS OF ELECTRONIC EQUIPMENT WITH A SHORT ACTION TIME

Vasil’ev E.N., Derevyanko V.A., Chebotarev V.E.

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