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100   $a20111115j198101    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFlight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane /$fFrank J. Kurtenbach and Frank W. Burcham, Jr
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dJanuary 1981.
215   $a1 online resource (18 pages) $cillustrations
225 1 $aNASA technical paper ;$v1782
300   $aTitle from title screen (viewed on Aug. 25, 2016).
300   $a"January 1981."
300   $a"Performing Organization: NASA Dryden Flight Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 18).
606   $aAfterburning$2nasat
606   $aF-15 aircraft$2nasat
606   $aJet thrust$2nasat
606   $aPressure measurement$2nasat
606   $aTurbofan engines$2nasat
606   $aAirplanes$xMotors$xThrust$2fast
606   $aFighter planes$xTurbojet engines$2fast
606   $aJet propulsion$2fast
615  7$aAfterburning.
615  7$aF-15 aircraft.
615  7$aJet thrust.
615  7$aPressure measurement.
615  7$aTurbofan engines.
615  7$aAirplanes$xMotors$xThrust.
615  7$aFighter planes$xTurbojet engines.
615  7$aJet propulsion.
700   $aKurtenbach$b Frank J.$01407186
702   $aBurcham$b Frank W.
712 02$aHugh L. Dryden Flight Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707439203321
996   $aFlight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane$93487858
997   $aUNINA