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2002
1Bezymyannyi Yu.G, 1Borovik VG, 2Galas' MI, 1Trefilov VI, 1Frolov GA. Feasibility of the ultrasound checking of the first-stage engine of the Zenith rocket carrier. 2. Results of the ultrasound diagnostics of the engine defectiveness. Kosm. nauka tehnol. 2002 ;8(1):032-036.
1Grachev EA, 1Grigoryan OP, 2Kudela K, 3Petrov AN, 3Sheveleva VN. Height distribution of electron fluxes with energies above 40 keV at mid-latitudes. Kosm. nauka tehnol. 2002 ;8(Supplement2):055-064.
1Grachev EA, 1Grigoryan OP, 2Kudela K, 3Petrov AN, 3Sheveleva VN. Height distribution of electron fluxes with energies above 40 keV at mid-latitudes. Kosm. nauka tehnol. 2002 ;8(Supplement2):055-064.
1Brovko MV, 1Golubek AV, 1Emelianova IA, 1Khorolskyi PG. Investigation and method development of quality estimate of catalogues of space object motion parameters. Kosm. nauka tehnol. 2002 ;8(Supplement1):073-077.
1Gotynyan OE, 1Ivchenko VM, 2Rapoport Yu.G, 3Parrot M. Ionospheric disturbances excited by the lithospheric gas source of acoustic gravity waves before eartquakes. Kosm. nauka tehnol. 2002 ;8(Supplement2):089-105.
1Nokel VP, 1Nikolaenko VM, 1Yampolsky Yu.S, 1Mamedov KYa., 1Venediktov Yu.I, 2Shuvalov VA, 3Dovgal SG, 4Gdalevich GL. Measuring system for direct determination of plasma parameters based on a symmetric dual Langmuir probe (SDLC). Kosm. nauka tehnol. 2002 ;8(Supplement2):207-212.
1Gudramovych VS. Methods for calculating the strength of rocket-space shell structures under local loading and contact interactions. Kosm. nauka tehnol. 2002 ;8(4):011-024.
1Baranskii PI, 1Babich VM, 2Svechnikov SV, 3Gaidar GP, 4Ptushynskyi Yu.G. Microgravity and ultrahigh vacuum as specific components of technological environment and new feasibilities of semiconductor technology. Kosm. nauka tehnol. 2002 ;8(4):096-099.
1Bessalyi VG, 2Gan B, 3Dzhur EA, 4Fesenko AG, 4Prikhod'ko VE. Microplasma welding of plateful silphons. Kosm. nauka tehnol. 2002 ;8(Supplement1):106-107.
1Satokin VV, 1Kharchenko VN, 1Tonkonozhenko AM, 1Gamaza EA. Mining computer program development of system "housing – filling compound" strength design analysis of space launchers solid propellant engines. Kosm. nauka tehnol. 2002 ;8(Supplement1):049-051.

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