LEADER 03368nam 2200637 a 450 001 9910817251603321 005 20230721020438.0 010 $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(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$b[electronic resource] $etesting and development practices in Russia /$fMark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley 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 $a1-56347-921-4 320 $aIncludes bibliographical references and index. 327 $aIntroduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. 410 0$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$01636210 701 $aYang$b Vigor$0322720 701 $aCulick$b F$g(Fred),$f1933-$01636211 701 $aTalley$b Douglas G$01636212 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910817251603321 996 $aCombustion instabilities in liquid rocket engines$93977373 997 $aUNINA