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Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit
Koroleva Y.L., Hohlov A.I., Nikolaev D.A., Borisova N.V., Mathynenko M.G.
Development of workspace and algorithms for testing SpaceWire onboard equipment
Maksyutin A.S., Murygin A.V., Ivlenkov D.V., Dymov D.V.
Methodology for calculating the de-weighting system of large-sized transformable elements of space vehicles for ground tests
Belyaev A.S., Filipas A.A., Tsavnin A.V., Tyryshkin A.V.
Small satellites for sea surface sounding
Kartsan I.N., Zhukov A.O.
Development of the CYCLOPS CubeSat payload
Sotnikova N.V., Kadadova A.V., Utkin V.V., Kadochnikov D.M.
Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit
Koroleva Y.L., Hohlov A.I., Nikolaev D.A., Borisova N.V., Mathynenko M.G.
MECHANISM OF OPERATED TELEMETRY FOR A SPACECRAFT
Lukin F.A., Shakhmatov A.V., Mushovets K.V., Zelenkov P.V.
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.
Simulationof onboard computer on the basis of open source IP-cores for small and ultra small space vehicles
Chekmarev S.A., Vergazov M.Y., Lukin F.A., Khanov V.K., Shakhmatov A.V., Chekmaryov S.A., Vergazov M.Y., Lukin F.A., Khanov V.K., Shahmatov A.V.
CYANATE ESTER COUPLING AGENTS IN AEROSPACE INDUSTRY. CATALYTIC PROPERTIES OF ORGANOMETALLIC COMPLEXES AND DIAZONIUM SALTS WITH COMPLEX ANIONS IN THE CURING REACTION OF CYANATE ESTER COUPLING AGENTS
Aristov V.F., Khalimanovich V.I., Mironovich V.V., Islentyeva T.A., Gurov D.A.
Perfection of control systems of space vehicles
Krushenko G.G., Golovanova V.V.
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.
Some units spacecraft balancing
Krushenko G.G., Golovanova V.V.
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.
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.
NANO MODIFICATION OF POLYMER BINDER WITH THE AIM OF IMPROVING THE PROPERTIES OF CARBON FIBRE MATERIALS
Krushenko G.G., Iseeva O.A.
PRINCIPLES OF ON-BOARD CONTROL COMPLEX DEVELOPMENT FOR SMALL SPACECRAFTS
Khanov V.K., Shakhmatov A.V., Chekmaryov S.A., Vergazov M.Y., Lukin F.A.
Container for transportation of the nuclear energy installation of a space vehicle
Dvirnyi V.V., Dvirnyi G.V., Krushenko G.G.
IMPROVEMENT OF SPACECRAFT MIRROR ANTENNA AND ELECTRONIC CIRCUIT BOARDS RELIABILITY
Dvirniy V.V., Morozov E.A., Dvirniy G.V., Krushenko G.G., Karaban V.M.
NETWORK ARCHITECTURE OF SPACECRAFT ON-BOARD EQUIPMENT MATING
Shahmatov A.V., Vergazov M.Y., Chekmaryov S.A., Khanov V.K.
DEVELOPMENT OF THE INFORMATION EXCHANGE SYSTEM EQUIPMENT FOR THE SMALL SPACECRAFT ONBOARD CONTROL UNIT
Khanov V.K., Shahmatov A.V., Chekmaryov S.A., Vergazov M.Y., Lukin F.A.
1 - 21 of 21 Items

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