LEADER 01165nam 2200325Ia 450 001 996383832103316 005 20221107235650.0 035 $a(CKB)1000000000598108 035 $a(EEBO)2240920454 035 $a(UnM)99122489700971 035 $a(EXLCZ)991000000000598108 100 $a19860130d1682 uy | 101 0 $aeng 135 $aurbn||||a|bb| 200 14$aThe parallel, or, The new specious association an old rebellious covenant$b[electronic resource] $eclosing with a disparity between a true patriot and a factious associator 210 $aLondon $cPrinted for B. Tooke ... and T. Sawbridge ...$d1682 215 $a[2], 34 p 300 $aWritten by John Northleigh. Cf. BM. 300 $aReproduction of original in Union Theological Seminary Library, New York. 330 $aeebo-0160 607 $aGreat Britain$xChurch history$y17th century 700 $aNorthleigh$b John$f1657-1705.$01003290 801 0$bEAA 801 1$bEAA 801 2$bm/c 801 2$bWaOLN 906 $aBOOK 912 $a996383832103316 996 $aThe parallel: or, The new specious association an old rebellious covenant$92306200 997 $aUNISA LEADER 01974nam 2200553 a 450 001 9910781420203321 005 20230421050641.0 010 $a1-60086-637-9 010 $a1-60086-418-X 035 $a(CKB)2550000000073082 035 $a(EBL)3111646 035 $a(SSID)ssj0000646560 035 $a(PQKBManifestationID)12215945 035 $a(PQKBTitleCode)TC0000646560 035 $a(PQKBWorkID)10698903 035 $a(PQKB)11725789 035 $a(Au-PeEL)EBL3111646 035 $a(CaPaEBR)ebr10516751 035 $a(OCoLC)922979061 035 $a(MiAaPQ)EBC3111646 035 $a(EXLCZ)992550000000073082 100 $a20120113d1995 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aLiquid rocket engine combustion instability$b[electronic resource] /$fedited by William E. Anderson and Vigor Yang 210 $aWashington, D.C. $cAmerican Institute of Aeronautics and Astronautics, Inc.$d1995 215 $a1 online resource (580 p.) 225 1 $aProgress in astronautics and aeronautics ;$vv. 169 300 $aDescription based upon print version of record. 311 $a1-56347-183-3 320 $aIncludes bibliographical references and index. 327 $apt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology. 410 0$aProgress in astronautics and aeronautics ;$vv. 169. 606 $aLiquid propellant rockets 606 $aRocket engines$xCombustion 615 0$aLiquid propellant rockets. 615 0$aRocket engines$xCombustion. 676 $a629.47522 701 $aYoung$b Vigor$01532860 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910781420203321 996 $aLiquid rocket engine combustion instability$93779385 997 $aUNINA