Volume 5, No. 4(38), 2021

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Dremukhin M.A., Nagovitsin V.N.
Development and modeling of non-metallic form-forming rigger for manufacture of polymer composition reflectors for satellite antennas

Kabanov S.A., Kabanov D.S.
Optimal deployment of the spoke of a largesized transformable reflector according to the hierarchy of criteria

Korotkov E.B., Shirobokov O.V., Matveev S.A., Yudina Z.A.
Overview of electric pump units for spacecraft thermal control systems

Ivanov A.V., Zommer S.A.
Analysis of the umbrella-type reflector opening process on a stand with an active gravity compensation system

Zhukov Yu.A., Korotkov E.B., Matveev S.A., Slobodzyan N.S., Shirobokov O.V.
Protection of precision spacecraft equipment from internal sources of vibration

Avtonomov N.N., Tololo A.V.
Determination of the optimum ball radius for researching materials using ball indenting

Sibiryakov A.V.
Wave theory of the laminated plates with approximate consideration of the transverse shear

Gubarev A.D., Yaschuk I.L., Khilinskaya Ya.V.
The reliability evaluation of the water surface remote monitoring satellite equipment

Volume 5, No. 3(37), 2021

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Kazantsev Z.A., Eroshenko A.M., Babkina L.A., Lopatin A.V.
Analysis of design of spacecraft solar arrays

Volkov M.V.
Modernization of the electromechanical equipment the trigger device: description of the design and testing

Mitin F.V., Nikulin E.N.
Modeling the deployment of a two-link spoke of a large-sized space reflector taking into account the backlash

Ledkova T.A., Zabolotnov Yu.M.
Analysis of the process of deployment of a lunar tether system taking into account the Earth's gravity

Volkov M.V., Dvirny V.V.
Solar battery frame made of pipes triangular cross-section

Kovel A.A.
Stages of information support of development of on-board equipment for spacecraft

Volume 5, No. 2(36), 2021

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Yudina Z.A., Sinichenko M.I., Ladigin A.P., Sin'kovskiy F.K., Usmanov D.B.
The vibration origin in the electric pump of the spacecraft and methods to reduce them

Popov I.P.
Elements of ballistic calculation for spacecraft gravity assist

Yudina Z.A., Sinichenko M.I., Ladigin A.P., Sin'kovskiy F.K., Kuznetsov A.D.
Valve for two-phase fluid loop

Gornostaev A.I.
Features of ensuring noise immunity of interface modules for temperature control in measuring instruments of spacecraft

Kovalev R.B., Kornienko V.V., Ratushnak V.N.
Estimation of the synchronization error for spaced-apart ground points of satellite communication

Blinov V.V., Vladimirov V.M., Kulinich S.N., Nikiforov A.I., Pridachin D.N., Pchelyakov D.O., Pchelyakov O.P., Sokolov L.V., Yarockiy D.V.
Equipment for growing semiconductor heterostructures in outer space

Volume 5, No. 1(35), 2021

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Basharina T.A., Goncharov M.G., Lymich S.N., Levin V.S., Shmatov D.P.
Low-thrust liquid-propellant rocket engines as part of advanced ultralight rocket vehicle systems

Taygin V.B., Lopatin А.V.
The review of designs of mirror spacecraft antennas with solid high precision size stable reflector

Lu H., Wang C., Zabolotnov Yu.M.
Dynamic analysis and motion control of spinning tether system during its Earth to Mars flight

Zommer S.A., Nemchaninov S.I., Kravchunovsky A.P., Ivanov A.V., Rudenko M.S.
Minimization of excess torque in multi-time deployment-folding hinge joints

Leonidov N.V.
Autonomous algorithms for monitoring the integrity of the navigation field in relation to GNSS GLONASS

Chebotarev V.E., Zimin I.I., Vnukov A.A.
Research of the ranges of effective application of unified space platforms for geostationary communication satellites