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100   $a19871030j196812    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffects of steady-state acceleration on combustion characteristics of an aluminized composite solid propellant /$fby G. Burton Northam
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1968.
215   $a1 online resource (41 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4914
300   $a"December 1968."
320   $aIncludes bibliographical references (page 14).
606   $aCombustion$2nasat
606   $aAcceleration (physics)$2nasat
606   $aSolid propellants$2nasat
606   $aAcceleration (Mechanics)$2fast
606   $aSolid propellant rockets$2fast
615  7$aCombustion.
615  7$aAcceleration (physics)
615  7$aSolid propellants.
615  7$aAcceleration (Mechanics)
615  7$aSolid propellant rockets.
700   $aNortham$b G. Burton$01396392
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bUAU
801  1$bUAU
801  2$bEGM
801  2$bAD#
801  2$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910715909503321
996   $aEffects of steady-state acceleration on combustion characteristics of an aluminized composite solid propellant$93456425
997   $aUNINA