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101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn engineering optimization method with application to STOL-aircraft approach and landing trajectories /$fby Heinrich G. Jacob
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1972.
215   $a1 online resource (iii, 38 pages) $cillustrations
225 1 $aNASA/TN ;$vD-6978
300   $a"September 1972."
300   $aPrepared at Ames Research Center.
320   $aIncludes bibliographical references (page 38).
606   $aV/STOL aircraft$2nasat
606   $aTrajectories$2nasat
606   $aAirplanes$xLanding
606   $aShort take-off and landing aircraft
606   $aAirplanes$xLanding$2fast
606   $aShort take-off and landing aircraft$2fast
606   $aTrajectory optimization$2fast
615  7$aV/STOL aircraft.
615  7$aTrajectories.
615  0$aAirplanes$xLanding.
615  0$aShort take-off and landing aircraft.
615  7$aAirplanes$xLanding.
615  7$aShort take-off and landing aircraft.
615  7$aTrajectory optimization.
700   $aJacob$b Heinrich G.$01422219
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aAmes Research Center.
801  0$bABC
801  1$bABC
801  2$bAD#
801  2$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716584403321
996   $aAn engineering optimization method with application to STOL-aircraft approach and landing trajectories$93545879
997   $aUNINA