LEADER 01661oam  2200481   450 
001 9910715048203321
005 20210107074505.0
035   $a(CKB)5470000002507522
035   $a(OCoLC)761196833
035   $a(OCoLC)995470000002507522
035   $a(EXLCZ)995470000002507522
100   $a20111115j196809    uy             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLoad relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements /$fby Leslie L. Scalzott and Fred Teren
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1968.
215   $a1 online resource (ii, 39 pages) $cillustrations
225 1 $aNASA technical note ;$vD-4786
320   $aIncludes bibliographical references (page 39).
606   $aAutomatic pilot (Airplanes)
606   $aAerospace vehicles$2nasat
606   $aLaunch vehicles$2nasat
606   $aAutomatic pilots$2nasat
615  0$aAutomatic pilot (Airplanes)
615  7$aAerospace vehicles.
615  7$aLaunch vehicles.
615  7$aAutomatic pilots.
700   $aScalzott$b Leslie L.$01416786
702   $aTeren$b Fred
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910715048203321
996   $aLoad relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements$93523334
997   $aUNINA