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Ensuring the thermal regime of spacecraft structures
Shatrov A., Rabetskaya O., Fisenko E.
On an alternative method for testing the dynamic strength of a small space-craft structure
Igolkin A., Filipov A.
Characteristics research of a low thrust rocket engine manufactured using additive SLM technology
Akbulatov E., Nazarov V., Gerasimov E.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y., Ivanov I., Tolstykh A., Islentev E.
On the issue of hydrodynamic braking efficiency while high-speed testing on a rocket-rail track
Astakhov S., Biryukov V., Kataev A.
Parameters of rocket engine chambers, obtained by selective laser fusion
Zhuravlev V., Manokhina E., Shinkarev M.
Features of achievement of limiting speed values of track tests of ballistic type aircraft
Astakhov S.
Automated system for detecting anomalies of periodic electrical signals
Krasnenko S., Khaidukova V., Nedorezov D.
Additional screening tests at the testing technical center for ground power equipment
Aliseenko Y., Nesterishin M., Vorontsova E., Fedosov V., Panteleev V.
Development of a mobile device for collection of heat power parameters of the refrigerator
Shurinova D., Suvorov A., Kovalenko A., Murygin A.
Methodology for assessing reliability of stand-bed systems in testing liquid throat engines
Nazarov V., Piunov V., Kolomentsev A., Yatsunenko V., Golikovskaya K.
Development of interface module emulator architecture for spacecraft life support systems
Komarov V., Semkin P.
Automated stand for electrical testing and diagnostics of life characteristics of lithium-ion batteries
Kopylov E., Lobanov D., Mizrah E.
Specialized LED assembly for out-atmospheric solar simulator
Shevchuk A., Dvirnyi V., Maybakh M., San'ko S., Pavlova A.
Alternative method of solar simulation for thermal vacuum tests of spacecraft
Shevchuk A.
Testing of spacecraft orientation and stabilization systems sing starry sky simulators
Gorelko M., Murygin A.
Characteristics of low thrust liquid-propellant rocket engines testing process
Nazarov V., Piunov V., Yatsunenko V., Savchin D.
Development of interface module emulator architecture for spacecraft life support systems
Komarov V., Semkin P.
Algorithm for simulation of vibration effects during track tests of aircraft and missile technology
Astakhov S., Biryukov V., Borovikov D.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y., Ivanov I., Tolstykh A., Islentev E.
Modeling and verification of working process parameters in gas generators for pressurizing fuel tanks of liquid propellant rocket propulsion systems
Sheludko M., Nazarov V., Zenyuk K., Nazarova L.
Problematic issues of application of methods of accelerated radiation testing of ECB
Avdyushkin S., Maximov I., Kochura S.
The shock-absorber for executive powers of system of stabilisation of a spaceCRAFT
Vasiltsov A., Lipovtsev A.
Conversion use of models of working processes of rocket engine turbine installations in the application to local power engineering
Abroskin V., Chernorot V., Kishkin A., Delkov A., Zhuravlev V.
SOLAR SIMULATORS FOR THERMAL VACUUM TESTS OF SPACECRAFT
Aslanyan R., Anisimov D., Marchenko I., Panteleev V.
Automated control system of heat fluxes at thermovacuum testing of spacecrafts
Shevlyakov A., Vykhristyuk I., Verkhoglyad A., Khalimanovich V., Hristich V.
The problems of the transform antennas manufacture and development
Dvirny G.
THEORETICAL BASES OF COMPOSITING TECHNIQUE OF LIGHT STREAMS FROM SEPARATE SOURSES OF RADIATION FOR SC LAND WORKING OFF
Krat S.
Testing of crimped electric connections in on-board DC harness of spacecraft for determination of their properties
Vasilyev I., Suntsov S., Efremov S., Kim V.
RESEARCH OF PARAMETERS VARIATIONS IMPACT ON THE STATIC ACCURACY OF SOLAR ARRAY SIMULATOR
Mizrah E., Shtabel N.
THE ALGORITHM FOR ESTIMATING ANGULAR RATE OF SPACECRAFT IN SURVIVABILITY MODE
Latyntsev S., Meus S., Оvсhinniкоv А.
Spacecraft structural test method based on kinematic excitation technique using verified finite element models
Dolgikh E., Arhipkin Y., Lysenko E., Lysenko К.
ASSESSMENT OF DETERMINATION ACCURACY OF EIGENTONES CHARACTERISTICS IN THE PRESENCE OF RANDOM ERRORS IN THE EXPERIMENTAL DATA
Bernc V., Berns V.
Mobile system weightlessness simulation for a large spacecraft
Kovalev I., Kikot J.
ORGANIZATION OF COMPLEX TESTING OF THE SPACECRAFT COMMAND AND MEASURING SYSTEM
Nozhenkova L., Isaeva O., Koldyrev A.
IMPROVEMENT OF INSULATION RESISTANCE MEASUREMENT ACCURACY DURING SPACECRAFT POWER SYSTEM TESTS
Shtabel N., Samotik L., Mizrah E.
ONGROUND TESTING OF SATELLITE ATTITUDE DETERMINATION AND CONTROL SYSTEM WITH THREE-AXIS MOTION SIMULATOR
Fedchenko D., Sinitskiy D.
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.
TECHNOLOGY OF OVERCOATING OF DESIGN ELEMENTS OF SPACE VEHICLES WITH ANTIEROSIVE COATING
Mikheev A., Girn A., Vakhteev E., Mikheev A., Evkin I., Girn A., Vakhteev E., Mikheev A., Evkin I.
Multi-headed star tracker 348K. Final in-earth validation results
Kareiln A., Zybin Y., Knyazev V., Pozdniakov A., Fomichev N.
METHODS OF PREPARATION OF THE EXPERIMENT FOR INVESTIGATION OF UNIVERSAL JOINTS ON NEEDLE BEARINGS
Eresko S., Eresko T., Kukushkin E., Menovshikov V., Orlov A.
On the static accuracy of charge-discharge units of one class intended for electrical tests of high capacity Li-ion batteries
Mizrah E., Lobanov D., Kopylov E., Balakirev R., Fedchenko A.
DETERMINATION OF MECHANICAL PROPERTIES OF MATERIALS OF HIGH PRESSURE METAL-XENON TANK
Aniskovich E., Seredin V.
DEVELOPMENT OF THE METHODOLOGY OF ELECTRIC THERMAL VACUUM TESTING FOR TEMPERATURE CONTROL OF SMALL SPACECRAFT JUBELEE-2 (MIR)
Vshivkov A., Golovenkin E., Krat S., Ganenko S.
SPACECRAFT THERMAL VACUUM OPTIMIZATION: DEVELOPMENT OF NEW TENDENCIES
Krat S., Khristich V., Krat S., Hristkh V.
TESTS OF SAMPLES RADIOREFLECTIVE COATINGS HARDINESS TO EXTERNAL FACTORS
Miheev A., Ivasev S., Kyzhetcov A., Bachkov I., Ravodina D.
ANALYSIS OF LED-BASED SOLAR SIMULATOR DEVELOPMENT CAPABILITY FOR SPACECRAFT GROUND TESTING APPLICATIONS
Dvirniy G., Shevchuk A., Dvirniy V., Elfimova M., Krushenko G.
ANALYSIS OF SOFTWARE FOR AUTOMATIC PERFORMANCE OF SPACECRAFT TESTS
Khasanova R.
SPACEСRAFT THERMAL VACUUM TESTING: AN EXPERIENCEOF CREATION OF SUNLIGHT SIMULATOR BASEDON THE HIGH-PRESSURE GAS-DISCHARGE LAMPS
Krat S., Filatov A., Khristich V., Krat S., Filatov A., Hristich V.
ELASTIC FEED SYSTEMS OF FUEL TANKS
Platov I.
IMPROVEMENT OF THE METHOD OF DETERMINING CAVITATION CHARACTERISTICS OF THE CENTRIFUGAL PUMPS
Nazarov V., Nazarova L., Shvetsova D., Savchin D.
AUTOMATED SIMULATION SYSTEM OF ELECTRICAL CHARACTERISTICS OF SPACECRAFT POWER SYSTEM
Mizrah E., Poymanov D., Balakirev R., Tkachev S.
Approach to select of universal vibratory system
Semenova L., Lysenko E., Lysenko K., Semenova L., Lysenko E., Lysenko K.
SPACECRAFT APPLICATION OF THREE LAYER HONEYCOMB STRUCTURES
Testoedov N., Nagovitsin V., Permyakov M.
GAPS CONTROL IN MOVABLE JOINTS BY THE RESULTS OF RESONANCE TEST
Berns V., Dolgopolov A.
AN APPROACH TO GROUND TESTING OF ROCKETS AND SPACE VEHICLES ON TRANSIENT PROCESSES BY COPRA-SPRING STAND
Bondarenko A., Mitin A., Tolchenov V., Eykhorn A., Yuranev O.
REACTION FLYWHEEL FOR THE SMALL SPACECRAFTS
Ermakov D., Denisova A., Kolevatova N., Gladyshev Y.
Increase of solar radiation simulator efficiency
Krat S., Krat S.
DEVELOPMENT AND IMPROVEMENT OF THE ON-BOARD CONTROL SYSTEM TEST METHODS AT TEST BENCH FACILITY
Golubev E., Nikolaev A.
ESTIMATION OF THE FROCINI CRITERIA AND OMEGA SQUARE CRITERIA STATISTICS BY THE STATISTICAL TESTS METHOD FOR A MIXTURE OF NORMAL DISTRIBUTIONS
Ushanov S., Ogurtsov D.
APPLICATION OF THE METHOD OF LOAD TESTING WITH GROUND experimental METHOD of CONTROL UNITS OF antenna GUIDANCE system
Kudryashova G., Babanov D., Galimzyanov A.
CREATION OF THE FUEL SILPHON TANKS MECHANICAL TEST MODES
Yermoshkin Y., Orlov S., Usanov A.
PHOTONIC SCHEMES MODELLING AND PARAMETRICAL OPTIMIZATION OF THE SUN SIMULATOR FOR THERMAL WORKING OF UNTIGHT SPACECRAFTS
Krat S., Filatov A., Dvirnyj V., Hristich V., Shatrov A.
Application FPGA for modelling of logic of functioning of spacecraft onboard radio-electronic equipment
Nedorezov D., Pichkalev A., Krasnenko S., Nepomnuashy O.
BUS-MODULAR SYSTEM FOR TEST OF ONBOARD RADIOELECTRONIC EQUIPMENT
Krasnenko S., Nedorezov D., Kashkin V., Pichkalev A.
VERIFICATION OF FINITE-ELEMENT MODEL SPACECRAFT VIA TEST RESULTS
Balyakov D.
PROPERTIES OF QUASICRYSTALLINE Al-Cu-Fe COATINGS PREPARED BY PLASMA SPRAYING
Lepeshev A., Karpov I., Ushakov A., Zelenkov P., Fedorov L.
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