LEADER 02293oam  2200649   450 
001 9910705842703321
005 20170802100021.0
035   $a(CKB)5470000002453991
035   $a(OCoLC)844613020
035   $a(EXLCZ)995470000002453991
100   $a20130526j199807    ua             0
101 0 $aeng
135   $aurcn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe high stability engine control (HISTEC) program $eflight demonstration phase /$fJohn C. DeLaat [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJuly 1998.
215   $a1 online resource (11 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v1998-208482
300   $a"July 1998."
300   $a"Prepared for the 34th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 12-15, 1998."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
300   $a"AIAA-98-3756."
320   $aIncludes bibliographical references (page 11).
517   $aHigh stability engine control 
606   $aEngine control$2nasat
606   $aGas turbine engines$2nasat
606   $aFlight tests$2nasat
606   $aF-15 aircraft$2nasat
606   $aFlow distortion$2nasat
606   $aReal time operation$2nasat
606   $aOn-line systems$2nasat
606   $aControl systems design$2nasat
606   $aInlet pressure$2nasat
606   $aStability augmentation$2nasat
615  7$aEngine control.
615  7$aGas turbine engines.
615  7$aFlight tests.
615  7$aF-15 aircraft.
615  7$aFlow distortion.
615  7$aReal time operation.
615  7$aOn-line systems.
615  7$aControl systems design.
615  7$aInlet pressure.
615  7$aStability augmentation.
700   $aDeLaat$b John C.$01406998
712 02$aLewis Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910705842703321
996   $aThe high stability engine control (HISTEC) program$93536428
997   $aUNINA