Experimental and computational studies of advanced two-phase thermal control systems for spacecraft and their elementsKhramov, Sergey Mikhailovich, 2003, Candidate of Sciences dissertation05.07.05 Thermal, electric-rocket engines and power plants of aircraftMoscow157 pp.Keywordsspacecraft thermal control systemsMore works in this specialtyDissertationSelection of energy-mass characteristics of reusable sustainer liquid-propellant rocket engines using liquefied natural gasKlepikov, Igor Alekseevich · 2005 · Doctor of Sciences · Bauman Moscow State Technical University05.07.05 Thermal, electric-rocket engines and power plants of aircraftDissertationNumerical and experimental investigation of the flow in the nozzle of a two-phase gas-droplet flow with a high mass concentration of liquid in the gasYakovlev, Aleksey Aleksandrovich · 2004 · Candidate of Sciences05.07.05 Thermal, electric-rocket engines and power plants of aircraftDissertationStudy of thermoacoustic heating of gas in gas-jet Hartmann generatorsLi Zhong Min · 2004 · Candidate of Sciences05.07.05 Thermal, electric-rocket engines and power plants of aircraftDissertationFriction and heat transfer in the boundary layer on a rough surfaceZhou Weixin · 2004 · Candidate of Sciences05.07.05 Thermal, electric-rocket engines and power plants of aircraftDissertationInfluence of the design parameters of a vortex pump on its energy characteristicsZhdanov, Igor' Leonidovich · 2004 · Candidate of Sciences05.07.05 Thermal, electric-rocket engines and power plants of aircraftAll works in this specialty