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100   $a20111121j196811    ua             0
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200 10$aResponse envelope $ea global description of three-axis large-angle spacecraft attitude control systems /$fby George Meyer
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dNovember 1968.
215   $a1 online resource (31 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4896
300   $a"November 1968."
320   $aIncludes bibliographical references (page 31).
517   $aResponse envelope 
606   $aControl$2nasat
606   $aAerospace sciences$2nasat
606   $aSpace vehicles$xAttitude control systems$2fast
615  7$aControl.
615  7$aAerospace sciences.
615  7$aSpace vehicles$xAttitude control systems.
700   $aMeyer$b George$f1934-$01387424
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bOCLCQ
801  2$bIYU
801  2$bGPO
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910715932803321
996   $aResponse envelope$93437252
997   $aUNINA

LEADER 02167nam  2200553I  450 
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100   $a20130128d2012      ua             0
101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 12$aA turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool /$fJeffrey T. Csank and Thomas J. Stueber
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012.
215   $a1 online resource (13 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217714
300   $aTitle from title screen (viewed on Jan. 14, 2013).
300   $a"September 2012."
300   $a"Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 30 to August 1, 2012."
300   $a"AIAA-2012-4149."
320   $aIncludes bibliographical references (pages 12-13).
606   $aComputerized simulation$2nasat
606   $aPropulsion system configurations$2nasat
606   $aWind tunnel tests$2nasat
606   $aFuel systems$2nasat
606   $aPropulsion system performance$2nasat
606   $aTurbine engines$2nasat
606   $aEngine inlets$2nasat
615  7$aComputerized simulation.
615  7$aPropulsion system configurations.
615  7$aWind tunnel tests.
615  7$aFuel systems.
615  7$aPropulsion system performance.
615  7$aTurbine engines.
615  7$aEngine inlets.
700   $aCsank$b Jeffrey T.$01402819
702   $aStueber$b Thomas J.
712 02$aNASA Glenn Research Center,
712 12$aJoint Propulsion Conference and Exhibit$d(48th :$f2012 :$eAtlanta, Ga.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702486003321
996   $aA turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool$93489481
997   $aUNINA