LEADER 01817nam  2200565I  450 
001 9910704683703321
005 20130610111754.0
035   $a(CKB)5470000002442875
035   $a(OCoLC)847518912
035   $a(EXLCZ)995470000002442875
100   $a20130610d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMissile aerodynamics for ascent and re-entry /$fG.L. Watts, J.W. McCarter
210  1$aHuntsville, Alabama :$cNational Aeronautics and Space Administration, Langley Research Center,$d2012.
215   $a1 online resource (ix, 13 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2012-217475
300   $aTitle from title screen (viewed on June 10, 2013).
300   $a"November 2012."
300   $a"Prepared for Marshall Space Flight Center."
606   $aAerodynamic characteristics$2nasat
606   $aAerodynamic forces$2nasat
606   $aAerodynamics$2nasat
606   $aAscent$2nasat
606   $aMathematical models$2nasat
606   $aDamping$2nasat
606   $aMissile configurations$2nasat
606   $aReentry$2nasat
606   $aSimulation$2nasat
615  7$aAerodynamic characteristics.
615  7$aAerodynamic forces.
615  7$aAerodynamics.
615  7$aAscent.
615  7$aMathematical models.
615  7$aDamping.
615  7$aMissile configurations.
615  7$aReentry.
615  7$aSimulation.
700   $aWatts$b G. L.$01413240
702   $aMcCarter$b J. W.
712 02$aGeorge C. Marshall Space Flight Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704683703321
996   $aMissile aerodynamics for ascent and re-entry$93509059
997   $aUNINA