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101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aOptimal pitch thrust-vector angle and benefits for all flight regimes /$fGlenn B. Gilyard, Alexander Bolonkin
210  1$aEdwards, California :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$dMarch 2000.
215   $a1 online resource (22 pages) $cillustrations
225 1 $aNASA/TM ;$v2000-209021
300   $a"March 2000."
300   $a"Performing organization: NASA Dryden Flight Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 22).
606   $aPitch (inclination)$2nasat
606   $aThrust vector control$2nasat
606   $aAutomatic flight control$2nasat
606   $aAngles (geometry)$2nasat
615  7$aPitch (inclination)
615  7$aThrust vector control.
615  7$aAutomatic flight control.
615  7$aAngles (geometry)
700   $aGilyard$b Glenn B.$01393171
702   $aBolonkin$b Alexander
712 02$aHugh L. Dryden Flight Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706239603321
996   $aOptimal pitch thrust-vector angle and benefits for all flight regimes$93454920
997   $aUNINA