LEADER 01452oam 2200421 450 001 9910717042803321 005 20220118104120.0 035 $a(CKB)5470000002527779 035 $a(OCoLC)1290170719 035 $a(OCoLC)995470000002527779 035 $a(EXLCZ)995470000002527779 100 $a20211227j197112 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aApplication of the steepest ascent optimization method to a reentry trajectory problem /$fby Bobby G. Junkin 210 1$aMarshall Space Flight Center, Alabama :$cGeorge C. Marshall Space Flight Center,$dDecember 1971. 215 $a1 online resource (approximately 110 pages) $cillustrations 225 1 $aNASA/TM ;$vX-64636 300 $a"December 10, 1971." 320 $aIncludes bibliographical references (page 102). 606 $aComputer programs$2nasat 606 $aOptimization$2nasat 606 $aTrajectory analysis$2nasat 615 7$aComputer programs. 615 7$aOptimization. 615 7$aTrajectory analysis. 700 $aJunkin$b Bobby G.$01396700 712 02$aGeorge C. Marshall Space Flight Center, 801 0$bGPO 801 1$bGPO 801 2$bGPO 906 $aBOOK 912 $a9910717042803321 996 $aApplication of the steepest ascent optimization method to a reentry trajectory problem$93512985 997 $aUNINA