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Title
Authors
Vol 15, No 4 (2014)
Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts
Delkov A.V., Hodenkov A.A., Shevchenko Y.N.
PDF
(Rus)
Vol 25, No 3 (2024)
Development of an experimental unit and methodology for ground-based experimental testing of two-phase thermoregulation systems for spacecrafts
Khodenkov A.A., Delkov A.V.
PDF
(Rus) PDF
(Eng)
Vol 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.Y., Tanasienko F.V., Golovenkin E.N., Yurtaev E.V.
PDF
(Rus)
Vol 24, No 3 (2023)
Ensuring the thermal regime of spacecraft structures
Shatrov A.K., Rabetskaya O.I., Fisenko E.N.
PDF
(Rus) PDF
(Eng)
Vol 20, No 3 (2019)
Calculation of complex heat transfer in the liquid circuit of the spacecraft thermal control system based on real topology and thermophysical properties
Shevchenko Y.N., Kishkin A.A., Tanasienko F.V., Shilkin O.V., Sokolov S.N.
PDF
(Eng)
Vol 19, No 3 (2018)
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.
PDF
(Rus)
Vol 20, No 3 (2019)
Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system
Shevchenko Y.N., Kishkin A.A., Tanasienko F.V., Shilkin O.V., Popugayev M.M.
PDF
(Eng)
Vol 21, No 3 (2020)
Study of impeller design parameters effect on the axial thrust of a centrifugal electric pump assembly
Kuznetsova Z.A., Sinichenko M.I., Kuznetsov A.D., Kleshnina I.A., Sin'kovskiy F.K.
PDF
(Eng)
Vol 21, No 3 (2020)
Development of the heat panel of the small space apparatus for navigation support
Kolga V.V., Yarkov I.S., Yarkova E.A.
PDF
(Eng)
Vol 16, No 2 (2015)
EXTENDING THE LIFE OF SATELLITE ON-BOARD UNITS
Testoedov N.A., Dvirnyi V.V., Morozov E.A., Dvirnyi G.V., Eremenko N.V.
PDF
(Rus)
Vol 11, No 4 (2010)
SPACECRAFT THERMAL VACUUM OPTIMIZATION: DEVELOPMENT OF NEW TENDENCIES
Krat S.A., Khristich V.V., Krat S.A., Hristkh V.V.
PDF
(Rus)
Vol 24, No 1 (2023)
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.
PDF
(Rus)
1 - 12 of 12 Items

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