LEADER 01616oam  2200457I  450 
001 9910705796603321
005 20190905115711.0
035   $a(CKB)5470000002452436
035   $a(OCoLC)227994156
035   $a(EXLCZ)995470000002452436
100   $a20080513d2002      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA comparison of different guidance schemes for a direct fire rocket with a pulse jet control mechanism /$fThanat Jitpraphai, Bradley Burchett, and Mark Costello
210  1$aAberdeen Proving Ground, MD :$cArmy Research Laboratory,$d2002.
215   $a1 online resource (vi, 21 pages) $cillustrations
300   $a"ARL-CR-493."
300   $a"April 2002."
320   $aIncludes bibliographical references (page 21).
606   $aRockets (Ordnance)
606   $aTrajectory optimization
606   $aPrecision guided munitions$zUnited States
615  0$aRockets (Ordnance)
615  0$aTrajectory optimization.
615  0$aPrecision guided munitions
700   $aJitpraphai$b Thanat$01415258
702   $aBurchett$b Bradley
702   $aCostello$b Mark
712 02$aU.S. Army Research Laboratory,
712 02$aOregon State University.$bDepartment of Mechanical Engineering.
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910705796603321
996   $aA comparison of different guidance schemes for a direct fire rocket with a pulse jet control mechanism$93516722
997   $aUNINA