LEADER 04429nam 2200673 a 450 001 9910955075903321 005 20251117094618.0 010 $a1-60086-690-5 010 $a1-60086-471-6 035 $a(CKB)2550000000072721 035 $a(EBL)3111571 035 $a(SSID)ssj0000551091 035 $a(PQKBManifestationID)12207230 035 $a(PQKBTitleCode)TC0000551091 035 $a(PQKBWorkID)10524488 035 $a(PQKB)10790345 035 $a(MiAaPQ)EBC3111571 035 $a(Au-PeEL)EBL3111571 035 $a(CaPaEBR)ebr10516675 035 $a(OCoLC)922978803 035 $a(BIP)15219132 035 $a(EXLCZ)992550000000072721 100 $a20101023d2007 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aCombustion instabilities in liquid rocket engines $etesting and development practices in Russia /$fMark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley 205 $a1st ed. 210 $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics$dc2007 215 $a1 online resource (342 p.) 225 1 $aProgress in astronautics and aeronautics ;$vv. 221 300 $aDescription based upon print version of record. 311 08$a1-56347-921-4 320 $aIncludes bibliographical references and index. 327 $aIntroduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. 330 $aThis is the first book in the literature to cover the development and testing practices for liquid rocket engines in Russia and the former Soviet Union.Combustion instability represents one of the most challenging probelms in the development of propulsion engines. A famous example is the F-1 engines for the first stage of the Saturn V launch vehicles in the Apollo project. More than 2000 full engine tests and a vast number of design modifications were conducted to cure the instability problem.This book contains first-hand information about the testing and development practices for treating liquid rocket combustion-instability problems in Russia and the former Soviet Union. It covers more than 50 years of research, with an emphasis placed on the advances made since 1970.The book was prepared by a former R&D director of the Research Institute of Chemical Engineering, NIICHIMMASH, the largest liquid rocket testing center in the world, and has been carefully edited by three well-known experts in the field. 410 0$aProgress in astronautics and aeronautics. 606 $aLiquid propellant rockets 606 $aRocket engines$xCombustion$zRussia (Federation)$xTesting 606 $aLiquid fuels$xCombustion$zRussia (Federation)$xTesting 606 $aRockets (Aeronautics)$zRussia (Federation)$xTesting 615 0$aLiquid propellant rockets. 615 0$aRocket engines$xCombustion$xTesting. 615 0$aLiquid fuels$xCombustion$xTesting. 615 0$aRockets (Aeronautics)$xTesting. 676 $a621.43/56 700 $aDranovsky$b Mark L$01871569 701 $aYang$b Vigor$0322720 701 $aCulick$b F$g(Fred),$f1933-$01871570 701 $aTalley$b Douglas G$01871571 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910955075903321 996 $aCombustion instabilities in liquid rocket engines$94480447 997 $aUNINA