Issue: 02'2018

02'2018 The journal presents the outcome of the Lavochkin Association activities aimed at development of a multipurpose FREGAT-SBU upper stage; the features of the first and subsequent domestic space astrophysics projects are shown; the issues of the efficiency improving of the modern Earth remote sensing space systems are covered as well as the strategy for development of space transportation systems to extraterrestrial sources of raw materials.

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Contents:

Lemeshevskii S.A., Ishin S.V., Asyushkin V.., Vikulenkov V.P., Shirshakov A.E., Fedoskin D.I., Efanov V.V., Yakovlev B.D., Jumahanov N.B., Poreshnev .Yu., Birukov A.S. Refined upper stage of FREGAT type designed for advanced medium class integrated launch vehicles (ILV)

Lemeshevskii S.A. Mathematical task description of design of the space systems for the Earth remote sensing considering the technology growth within the planned period

Lemeshevskii S.A. Methodological scheme of decomposition while solving of the task of the space systems for the Earth remote sensing design considering the technology growth within the planned period

Moisheev A.A. Creation of space segments of astrophysical observatories

Sachkov M.E., Savanov I.S., Shustov B.M., Shugarov A.S., Sichevskij S.G. Astrophysical space mission for all-sky survey in ultraviolet spectral domain Astron-2

Panchuk V.E., Sachkov M.E., Klochkova V.G. Instrumentation for ground based astronomical support of the SPEKTR-UF mission

Lemeshevskii S.A., Graphodatsky O.S., Shirshakov A.E., Moskatiniev I.V., Mitkin A.S., Baliyev A.V. Space transport systems for industrial and scientific development of small celestial bodies

Golomazov M.M., Ivankov A.A. Examination of the aerodynamics of a prospective descent module descending in the atmosphere of Mars

Platov I.V., Simonov A.V. Rational flight scheme design of the mission spacecrafts to the centre of Solar system

Shevchenko S.N. Generation of target function at justification of optimal long-term development programs of spacecraft for social economy applications

Demenko O.G., Birukov A.S. Special features of verification for ExoMars-2020 Spacecraft Composite Descent Module shock strength

Belyaev B.B., Ulyashin A.I., Telepnev P.P. Features of operation reaction wheel used in precision stabilization of spacecraft

Lubomudrov .., Efanov V.V., Gorovtsov V.V., Kuzin .N. Electromagnetic interferences generated in the spacecraft at static-charge accumulation

Khamidullina N.., Artiomov .., Tyutyunnikov .. Estimation of the displacement damage effects in the radioelectronic equipment onboard ExoMars-2020 descent module

Volchenkov A.S., Petrov A.S., Prilutskiy A.A., Chikov V.A. Grating lobes in the space-borne sub-aperture antenna arrays

Khokhlachev E.N., Shakhanov A.E. Forecasting of costs in the early stages of space systems design

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