LEADER 01865nam  2200505   450 
001 9910707128703321
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035   $a(CKB)5470000002462213
035   $a(OCoLC)949276125
035   $a(EXLCZ)995470000002462213
100   $a20160510j199606    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign of a mixer for the thrust-vectoring system on the high-alpha research vehicle /$fW. Thomas Bundick [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJune 1996.
215   $a1 online resource (38 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110228
300   $aTitle from title screen (viewed on May 10, 2016).
300   $a"June 1996."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (pages 37-38).
606   $aControl systems design$2nasat
606   $aFlight simulation$2nasat
606   $aThrust vector control$2nasat
606   $aFlight control$2nasat
606   $aFlight tests$2nasat
606   $aVanes$2nasat
615  7$aControl systems design.
615  7$aFlight simulation.
615  7$aThrust vector control.
615  7$aFlight control.
615  7$aFlight tests.
615  7$aVanes.
700   $aBundick$b W. Thomas$01388929
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707128703321
996   $aDesign of a mixer for the thrust-vectoring system on the high-alpha research vehicle$93449889
997   $aUNINA