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100   $a20111114j196809    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPerformance and stability characteristics of nitrogen tetroxide - hydrazine combustors /$fby Martin Hersch
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1968.
215   $a1 online resource (ii, 20 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4776
300   $a"September 1968."
320   $aIncludes bibliographical references (pages 19-20).
606   $aRockets (Aeronautics)$xFuel$xCombustion
606   $aHydrazines
606   $aHydrazines$2fast
615  0$aRockets (Aeronautics)$xFuel$xCombustion.
615  0$aHydrazines.
615  7$aHydrazines.
700   $aHersch$b Martin$01395383
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910715048003321
996   $aPerformance and stability characteristics of nitrogen tetroxide - hydrazine combustors$93453802
997   $aUNINA