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100   $a20140916j196810    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines /$fby Reino J. Salmi, John P. Wanhainen, and Ned P. Hannum
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1968.
215   $a1 online resource (ii, 27 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4851
300   $a"October 1968."
320   $aIncludes bibliographical references (pages 26-27).
606   $aRocket engines$xCombustion
606   $aRocket engines$xThrust
606   $aRocket engines$xCombustion$2fast
606   $aRocket engines$xThrust$2fast
615  0$aRocket engines$xCombustion.
615  0$aRocket engines$xThrust.
615  7$aRocket engines$xCombustion.
615  7$aRocket engines$xThrust.
700   $aSalmi$b Reino J.$01395045
702   $aWanhainen$b John P.
702   $aHannum$b Ned P.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLewis Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910714071603321
996   $aEffect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines$93453007
997   $aUNINA