Іздеу

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)

Том 25, № 2 (2024)

Results of monitoring the radiation environment in medium circular orbit

Eliseev D., Grafodatsky O., Ivanov V., Maksimov I., Molchanov K., Prokopyev V.

(Rus)

(Eng)

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

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

(Eng)

Том 25, № 1 (2024)

Study of the payload extraction trajectory heavy class carrier rocket

Bordachev V., Kolga V.

(Rus)

(Eng)

Том 23, № 2 (2022)

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

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

(Rus)

Том 20, № 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)

Том 25, № 2 (2024)

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

Еsina P., Kornev V.

(Rus)

Том 22, № 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., Vnukov A., Volkov D., Kochev Y., Simanov R., Yakimov E., Grikhin G.

(Rus)

(Eng)

Inter-satellite optical communication link

Aleksandrov A., Vasilenko A., Korolev D.

(Eng)

Том 21, № 4 (2020)

On remote sensing of the earth by spacecraft

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

(Eng)

Том 22, № 1 (2021)

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

Kartsan I., Efremova S.

(Rus)

(Eng)

Том 25, № 1 (2024)

Calculation of the coupling loss factors for the angle connected beams

Kravchunovky A.

(Rus)

(Eng)

Том 21, № 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)

Том 21, № 3 (2020)

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

Kolga V., Yarkov I., Yarkova E.

(Eng)

Том 23, № 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)

Том 22, № 4 (2021)

Development of workspace and algorithms for testing SpaceWire onboard equipment

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

(Rus)

(Eng)

Том 25, № 1 (2024)

Issues of ensuring the resistance of high-voltage solar arrays of spacecraft to the effects of secondary arc discharges

Valiullin V., Kochura S., Maximov I., Nadiradze A.

(Rus)

(Eng)

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

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

(Eng)

Том 23, № 2 (2022)

Small satellites for sea surface sounding

Kartsan I., Zhukov A.

(Rus)

Том 20, № 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)

Том 22, № 4 (2021)

Alternative method of solar simulation for thermal vacuum tests of spacecraft

Shevchuk A.

(Rus)

(Eng)

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

Savenkov V., Tishchenko A., Volokitin V.

(Eng)

Том 23, № 4 (2022)

Testing of spacecraft orientation and stabilization systems sing starry sky simulators

Gorelko M., Murygin A.

(Rus)

Ground control system for distant space vehicles

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

(Rus)

Development of interface module emulator architecture for spacecraft life support systems

Komarov V., Semkin P.

(Eng)

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

Kravchunovky A.

(Rus)

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

Savenkov V., Tishchenko A., Volokitin V.

(Eng)

Том 22, № 1 (2021)

Methodology for calculating the de-weighting system of large-sized transformable elements of space vehicles for ground tests

Belyaev A., Filipas A., Tsavnin A., Tyryshkin A.

(Rus)

(Eng)

Implementation of “digital twin” technology within the thermo-elastic distortion testing of a precision carbon fiber reflector for the spacecraft antenna subsystem

Ivanov A.

(Rus)

Development of interface module emulator architecture for spacecraft life support systems

Komarov V., Semkin P.

(Eng)

Problematic issues of application of methods of accelerated radiation testing of ECB

Avdyushkin S., Maximov I., Kochura S.

(Rus)

Inter-satellite optical communication link

Aleksandrov A., Vasilenko A., Korolev D.

(Eng)

Development concept of inter-satellite laser communication

Kartsan I.

(Rus)

Том 17, № 3 (2016)

GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD

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

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)

Development of the CYCLOPS CubeSat payload

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

(Rus)

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

Nazarenko A., Maximov I., Kochura S.

(Rus)

INVESTIGATION OF CHARGE-DISCHARGE PROCESSES IN THE SPACECRAFT DETACHABLE CONNECTOR

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

(Rus)

Том 12, № 3 (2011)

ADAPTIVE MULTI BEAM ANTENNA JSC «ISS»

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

(Rus)

Том 10, № 5 (2009)

Geo satellite attitude and orbit control: fixed orbit control thrasters

Ermoshkin Y., Raevsky V., Urusov V.

(Rus)

Том 13, № 2 (2012)

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

Dvirniy G.

(Rus)

Том 12, № 2 (2011)

Electric propulsions rational application range on the applied spacecrafts

Ermoshkin Y., Yermoshkin Y.

(Rus)

Том 11, № 2 (2010)

MODERN SPACECRAFTS OPERATIONAL RELIABILITY AND QUALITY ANALYSIS

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

(Rus)

Том 15, № 1 (2014)

Rational photovoltaic batteries mounting on the earth remote sensing microsatellite

Gubin S., Shepetov Y., Dolzhukova K.

(Rus)

Том 15, № 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)

Том 19, № 1 (2018)

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

Kolovsky I., Shmakov D., Podolyakin V.

(Rus)

Том 18, № 1 (2017)

THE EVOLUTION OF THE PROJECT “SEA LAUNCH” OF SPACECRAFT

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

(Rus)

Том 18, № 1 (2017)

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

Deev P., Sinkovskiy F.

(Rus)

Том 17, № 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.

Том 16, № 1 (2015)

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

Vasiltsov A., Lipovtsev A.

(Rus)

Том 11, № 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)

Том 10, № 4 (2009)

GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS

Yermoshkin Y., Raevsky V., Urusov V.

(Rus)

Том 13, № 5 (2012)

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

Kislitskiy M.

(Rus)

Том 12, № 1 (2011)

CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT

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

(Rus)

Том 11, № 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)

Том 15, № 4 (2014)

Mobile system weightlessness simulation for a large spacecraft

Kovalev I., Kikot J.

(Rus)

Том 15, № 1 (2014)

Unification methods of present telemetry processing systems in satellite control centers

Nekrasov M., Packman D., Antamoshkin A.

(Rus)

Том 14, № 3 (2013)

MICROELECTRONIC SYSTEMS FOR AUTOMATION OF PERSPECTIVE SPACE VEHICLES

Nepomnuashy O., Ohotkin K., Habarov V.

(Rus)

Том 14, № 3 (2013)

DEVELOPMENT OF COMPOSITE PRECISION SATELLITE REFLECTOR: FINITE ELEMENT CONSTRUCTION MODELING

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

(Rus)

Том 19, № 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)

Том 18, № 3 (2017)

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)

Том 17, № 4 (2016)

ASSESSMENT OF SPACECRAFT SOLAR ARRAY RELIABILITY DURING GROUND EXPERIMENTAL DEVELOPMENT TEST

Zakharov S.

Том 16, № 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)

Том 10, № 5 (2009)

Development of mechanical test procedure for the fuel bellows tanks

Ermoshkin Y., Orlov S., Usanov A.

(Rus)

Том 13, № 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)

Том 12, № 1 (2011)

UPGRADING OF PHOTOVOLTAICARRAY SIMULATORWITH TWO-CIRCUIT CONTROL ELEMENT

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

(Rus)

Том 16, № 2 (2015)

TOP-DOWN APPROACH FOR SPACECRAFT DEVELOPMENT

Lihachev M.

(Rus)

Том 15, № 2 (2014)

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

Nozhenkova L., Isaeva O., Gruzenko E.

(Rus)

Том 15, № 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)

Том 14, № 3 (2013)

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)

Том 19, № 3 (2018)

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

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

(Rus)

Том 18, № 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)

Том 17, № 3 (2016)

DOUBLE-CONIC ADAPTER FOR LAUNCHING THE BLOCK OF THREE SPACECRAFTS

Khakhlenkova A.

Том 17, № 3 (2016)

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

Shatov A., Khakhlenkova A.

Том 16, № 3 (2015)

REDUCTION OF SPACECRAFT HARNESS MASS

Dvirnyi V., Eremenko N., Dvirnyi G.

Том 10, № 5 (2009)

Implementation error of relative measurements

Garin E.

(Rus)

Том 11, № 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)

Том 17, № 1 (2016)

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

Kovalev I., Badanina J.

Том 15, № 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)

Том 14, № 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)

Том 14, № 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)

Том 19, № 4 (2018)

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

Chernaya M.

(Rus)

Том 19, № 1 (2018)

VERIFICATION OF FINITE-ELEMENT MODEL SPACECRAFT VIA TEST RESULTS

Balyakov D.

(Rus)

Том 18, № 3 (2017)

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

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

(Rus)

Том 17, № 4 (2016)

LATTICE CYLINDRICAL SHELL WITH A ROUND TRANSVERSE PROFILE AND VARIABLE STIFFNESS

Khakhlenkova A.

Том 17, № 2 (2016)

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

Khakhlenkova A., Shatov A.