Pesquisa

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 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 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)

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

Kravchunovky A.

(Rus)

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)

Volume 21, Nº 2 (2020)

Inter-satellite optical communication link

Aleksandrov A., Vasilenko A., Korolev D.

(Eng)

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

Avdyushkin S., Maximov I., Kochura S.

(Rus)

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 22, Nº 1 (2021)

Parametric analysis of the anisogrid body of the spacecraft for cleaning the orbit of space debris

Belonovskaya I., Kolga V., Yarkov I., Yarkova E.

(Rus)

(Eng)

Development concept of inter-satellite laser communication

Kartsan I.

(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)

Ground control system for distant space vehicles

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

(Rus)

Volume 23, Nº 4 (2022)

The feature of the “Express-AMU3”, “Express-AMU7” spacecrafts injecton to geostationary orbit

Ermoshkin Y., Vnukov A., Volkov D., Kochev Y., Simanov R., Yakimov E., Pridannikov S.

(Rus)

Volume 23, Nº 4 (2022)

Testing of spacecraft orientation and stabilization systems sing starry sky simulators

Gorelko M., Murygin A.

(Rus)

Volume 18, Nº 4 (2017)

THE ANALYSIS OF COMPLETED, ONGOING AND POTENTIAL MISSIONS TO THE JUPITER SYSTEM

Gordienko E., Platov I., Simonov A.

(Rus)

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

Nazarenko A., Maximov I., Kochura S.

(Rus)

Volume 16, Nº 1 (2015)

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

Vasiltsov A., Lipovtsev A.

(Rus)

Volume 18, Nº 2 (2017)

ANALYSIS OF CLEANING CONCEPTS OF NEAR-EARTH SPACE

Kirillov V., Bagateev I., Tarleckiy I., Balandina T., Balandin E.

(Rus)

Volume 13, Nº 4 (2012)

About domestic system of space monitoring of emergencies

Testoedov N., Dvirnyj V., Nosenkov A., Elfimova M.

(Rus)

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

Maximov I., Kochura S., Avdyushkin S.

(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 2 (2011)

Approach to select of universal vibratory system

Semenova L., Lysenko E., Lysenko K., Semenova L., Lysenko E., Lysenko K.

(Rus)

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 16, Nº 4 (2015)

SYSTEM FOR MONITORING THE LEVELS OF SPACE ENVIRONMENT EXPOSURE EXPERIENCED BY SATELLITES DEVELOPED BY “INFORMATION SATELLITE SYSTEMS” COMPANY

Testoedov N., Kochura S., Maximov I.

Volume 15, Nº 4 (2014)

Backgrounds and trends of all-electric propulsion geostationary satellites creation

Vnukov A., Rvacheva E.

(Rus)

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

Kuzovnikov A., Testoedov N., Agureev V.

(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)

Volume 19, Nº 3 (2018)

INCREASE RELIABILITY OF ULTRAHIGH-FREQUENCY CHANNELS OF THE ACTIVE PHASED ARRAY ANTENNA MODULES

Kartsan I., Shangina E., Kiselev G., Efremova S.

(Rus)

Volume 19, Nº 1 (2018)

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

Kolovsky I., Shmakov D., Podolyakin V.

(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)

ASSESSMENT OF SPACECRAFT SOLAR ARRAY RELIABILITY DURING GROUND EXPERIMENTAL DEVELOPMENT TEST

Zakharov S.

Volume 11, Nº 1 (2010)

Indicatrix account of materials dispersion at the estimations of erosion-contaminating influence of streams of plasma thrusters on space craft

Nadiradze A., Shaposhnikov V., Smirnov V., Maximov I., Kochura S.

(Rus)

Volume 10, Nº 3 (2009)

Testing laboratory patternswith thermoregulation coatings on carbon details of space vehicles

Khalimanovich V., Kharlamov V., Ermolaev R., Mikheev A., Girn 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 2 (2011)

Dual-use spacecraft conception

Kislitskiy M., Kislitsky M.

(Rus)

PROBLEMS OF SUPPORT OF RELIABLE OPERATION OF MODERN SC UNDER FACTORS OF SPACE AND TECHNOGENEOUS CHARACTER DESTABILISING INFLUENCE

Maksimov I., Maximov I.

(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)

Volume 14, Nº 3 (2013)

MICROELECTRONIC SYSTEMS FOR AUTOMATION OF PERSPECTIVE SPACE VEHICLES

Nepomnuashy O., Ohotkin K., Habarov V.

(Rus)

ONBOARD COMPUTER COMPLEX FOR UNPRESSURISED LONG-RESOURCED SPACECRAFTS

Kozlov I.

(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)

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 2 (2017)

SOLAR SIMULATORS FOR THERMAL VACUUM TESTS OF SPACECRAFT

Aslanyan R., Anisimov D., Marchenko I., Panteleev V.

(Rus)

Volume 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., Derevyanko V., Chebotarev V.

Volume 10, Nº 4 (2009)

CREATION OF THE FUEL SILPHON TANKS MECHANICAL TEST MODES

Yermoshkin Y., Orlov S., Usanov A.

(Rus)

Volume 10, Nº 1-1 (2009)

The problems of the transform antennas manufacture and development

Dvirny G.

(Rus)

Volume 13, Nº 2 (2012)

ADAPTIVE MULTIBEAM ANTENNAS

Tyapkin V., Pershin A., Dmitriev D., Moshkina T.

(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)

OPTIMIZATION OF WORKING OFF OF THE SPACE VEHICLE «JAMAL-300К»CREATED ON THE BASIS OF THE RECURRENT PLATFORM

Patraev V., Patraev V.

(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 1 (2014)

Unification methods of present telemetry processing systems in satellite control centers

Nekrasov M., Packman D., Antamoshkin A.

(Rus)

SEPARATION DEVICE FOR SPACECRAFT UNPRESSURIZED PLATFORMS BASED ON ISOGRID STRUCTURES

Vehov A.

(Rus)

Volume 14, Nº 3 (2013)

DEVELOPMENT OF COMPOSITE PRECISION SATELLITE REFLECTOR: FINITE ELEMENT CONSTRUCTION MODELING

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

(Rus)

MATHEMATICAL MODEL FOR GEOSTATIONARY SPACECRAFT DISTURBING TORQUES DETERMINATION

Latyntsev S., Murygin A.

(Rus)

MODELING OF SPECTROERERGETIC CHARACTERISTICS OF SPACE OBJECTS IN THE OPTICAL RANGE

Bogoyavlenskiy A., Kamenev A., Poluyan M., Soluyanov A.

(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)

GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD

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

Volume 16, Nº 1 (2015)

SATELLITE-BORNE MICROPROCESSOR CONTROL SYSTEM WITH IMPROVE UPSET TOLERANCE

Udalov D.

(Rus)

Volume 10, Nº 4 (2009)

THE DETERMINATION OF RELATIVE COORDINATES BASEDON THE RETRANSMISSION OF NAVIGATION SIGNALSOF THE GLONASS AND GPS SYSTEMS

Garin Е.

(Rus)

Volume 10, Nº 3 (2009)

Land control complex for small space vehicles

Kartsan I.

(Rus)

Volume 13, Nº 2 (2012)

DISTINCTIVE FEATURES OF MAINTENANCE OF FLAWLESNESS OF NONREUSABLE MECHANICAL DEVICES FUNCTIONING ON SPACE VEHICLES

Pokhabov Y.

(Rus)

Volume 12, Nº 1 (2011)

CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT

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

(Rus)

METHODS AND ALGORITHMS FOR MICROPROGRAM CONTROL OF HIGH-SPEED, IMPULSE VOLTAGE REGULATORS FOR POWER SUPPLY OF ONBOARD EQUIPMENT OF PERSPECTIVE SPACE VEHICLES

Veysov E., Nepomnyashchiy O., Krasnobaev Y., Kapulin D., Veysov Е., Nepomnyaschi О., Krasnobaev U., Kapulin D.

(Rus)

Volume 15, Nº 1 (2014)

Rational photovoltaic batteries mounting on the earth remote sensing microsatellite

Gubin S., Shepetov Y., Dolzhukova K.

(Rus)

Volume 14, Nº 3 (2013)

INVESTIGATION OF THE SPACE VEHICLES COATINGS FEATURES

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

(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)

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)

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., Simonov A.

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 12, Nº 3 (2011)

ADAPTIVE MULTI BEAM ANTENNA JSC «ISS»

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

(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 3 (2009)

Instrumental error of relative measurements

Garin E.

(Rus)

Volume 13, Nº 1 (2012)

FEATURES OF EXPERIMENTAL DEFINITION OF COMPOSITE MATERIALS DURABILITY AGAINST EROSIVE IMPACT OF STATIONARY PLASMA THRUSTERS

Nadiradze A., Rachmatullin R., Kochura S., Maksimov I., Smirnov V.

(Rus)

Volume 10, Nº 2 (2009)

ELECTRONIC EQUIPMENT OF SPACECRAFT AND THERMOANALYSIS OF PRINTED-CIRCUIT -BOARDS

Yutkin A., Klimkin O., Dzyuvina A.

(Rus)

Volume 16, Nº 2 (2015)

TOP-DOWN APPROACH FOR SPACECRAFT DEVELOPMENT

Lihachev M.

(Rus)

Volume 15, Nº 4 (2014)

Mobile system weightlessness simulation for a large spacecraft

Kovalev I., Kikot J.

(Rus)

Volume 14, Nº 4 (2013)

THE QUESTIONS OF TECHNICAL REALIZATION OF THE DYNAMIC BENCH FOR THE RESEARCH OF THE ACTIVITY OF THE ENGINE-FLYWHEEL OF THE ATTITUDE CONTROL SYSTEM AND SPACE VEHICLE STABILIZATION

Sinitskiy D., Murigin A.

(Rus)

Volume 14, Nº 1 (2013)

Estimation of the form of a large-sized transformed reflector surface for a spacecraft

Goldobin N.

(Rus)

Volume 19, Nº 3 (2018)

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

Chebotarev V., Zimin I.

(Rus)

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

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

(Rus)

Volume 18, Nº 4 (2017)

STRESS ANALYSIS OF SOLAR ARRAY DRIVER MECHANISM ACTUATOR OF THE SPACECRAFT “LUNA-RESURS-1”

Tambasova E., Tokarev A., Pavelko S., Таmbаsоv I.

(Rus)

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

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

(Rus)

Volume 17, Nº 3 (2016)

AUTOMATED SIMULATION SYSTEM OF ELECTRICAL CHARACTERISTICS OF SPACECRAFT POWER SYSTEM

Mizrah E., Poymanov D., Balakirev R., Tkachev S.

Volume 11, Nº 6 (2010)

UNTIGHTENED PLATFORM OF SPACE VEHICLE FOR REMOTESOUNDING OFTHE EARTH

Shangina E., Rybakov A., Pasechnik K., Zaytsev P., Vlasov A., Shangina E., Ribakov А., Pasechnik К., Zaytsev P., Vlasov A.

(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 10, Nº 1-2 (2009)

BUNDLED SOFTWARE TO COMPUTE TEMPERATURE FIELDS OF SPACE VEHICLES PANELS WITH LEAKY CONSTRUCTION

Vasiljev E., Derevyanko V.

(Rus)