LEADER 01686oam 2200493I 450 001 9910715018703321 005 20201130130826.0 035 $a(CKB)5470000002507820 035 $a(OCoLC)761778985 035 $a(EXLCZ)995470000002507820 100 $a20111121j196808 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAttitude determination of the spin-stabilized Project Scanner spacecraft /$fby T.M. Walsh, Jean C. Keating, and Dwayne E. Hinton 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dAugust 1968. 215 $a1 online resource (iii, 65 pages) $cillustrations 225 1 $aNASA technical note ;$vTN D-4740 300 $a"August 1968." 320 $aIncludes bibliographical references (page 41). 606 $aSpace vehicles$xAttitude control systems$xMeasurement 606 $aSpin (Aerodynamics) 606 $aSpin (Aerodynamics)$2fast 615 0$aSpace vehicles$xAttitude control systems$xMeasurement. 615 0$aSpin (Aerodynamics) 615 7$aSpin (Aerodynamics) 700 $aWalsh$b T. M.$01405661 702 $aKeating$b Jean C. 702 $aHinton$b Dwayne E. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 712 02$aLangley Research Center. 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCLCQ 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910715018703321 996 $aAttitude determination of the spin-stabilized Project Scanner spacecraft$93522062 997 $aUNINA