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100   $a20110224j199306    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExtraction of stability and control derivatives from orbiter flight data /$fKenneth W. Iliff and Mary F. Shafer
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dJune 1993.
215   $a1 online resource (46 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4500
300   $a"June 1993."
300   $a"Performing organization: NASA Dryden Flight Research Facility"--Report documentation page.
320   $aIncludes bibliographical references (pages 23-24).
606   $aAerodynamic stability$2nasat
606   $aFlight envelopes$2nasat
606   $aHypersonic flight$2nasat
606   $aSpace Shuttle orbiters$2nasat
606   $aStability derivatives$2nasat
615  7$aAerodynamic stability.
615  7$aFlight envelopes.
615  7$aHypersonic flight.
615  7$aSpace Shuttle orbiters.
615  7$aStability derivatives.
700   $aIliff$b Kenneth W.$013447
702   $aShafer$b Mary F.
712 02$aDryden Flight Research Facility.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
801  0$bSSN
801  1$bSSN
801  2$bGPO
906   $aBOOK
912   $a9910705736603321
996   $aExtraction of stability and control derivatives from orbiter flight data$93478762
997   $aUNINA