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Feasibility of the ultrasound testing of the first-stage engine of the Zenith rocket carrier. 1.Construction of the physical model of the object to be tested. Kosm. nauka tehnol. 2001 ;7(5-6):003-007.
. 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.
. Expert system for creation and optimization of aerospace materials. Kosm. nauka tehnol. 1995 ;1(2):60–64.
. Experimental modelling of heat modes of small space vehicles and their external heat flows. II. Heat vacuum test results of the MS-1-TK-TV -type micro-sputnik mock-up. Kosm. nauka tehnol. 2002 ;8(4):003-010.
. Excitation of meridional flow by differential rotation in Earth's liquid core. Kosm. nauka tehnol. 2000 ;6(2):53–68.
. Estimating the resonance oscillation regimes in space vehicles. Kosm. nauka tehnol. 2003 ;9(4):040-044.
. Estimate of the influence of thermophysical parameter deviations on spacecraft's thermal regime. Kosm. nauka tehnol. 2006 ;12(1):018-022.
. The essential results of the investigations performed on the Russian Segment of the International Space Station and the prospects for the realization of Russian experiments with the participation of Ukraine. Kosm. nauka tehnol. 2008 ;14(2):42-45.
. Equipment and technology for electron-beam welding in space. Space Science and Technology. 2017 ;23(4):27-32.
. Ensuring the information from a drill robot under the adaptive control of technological processes in space experiments. Kosm. nauka tehnol. 1999 ;5(4):22–27.
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