01661oam 2200481 450 991071504820332120210107074505.0(CKB)5470000002507522(OCoLC)761196833(OCoLC)995470000002507522(EXLCZ)99547000000250752220111115j196809 uy 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierLoad relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements /by Leslie L. Scalzott and Fred TerenWashington, D.C. :National Aeronautics and Space Administration,September 1968.1 online resource (ii, 39 pages) illustrationsNASA technical note ;D-4786Includes bibliographical references (page 39).Automatic pilot (Airplanes)Aerospace vehiclesnasatLaunch vehiclesnasatAutomatic pilotsnasatAutomatic pilot (Airplanes)Aerospace vehicles.Launch vehicles.Automatic pilots.Scalzott Leslie L.1416786Teren FredUnited States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCFOCLCQGPOBOOK9910715048203321Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements3523334UNINA