02344oam 2200589 450 991071608630332120210430133710.0(CKB)5470000002517238(OCoLC)785280955(OCoLC)761397300(EXLCZ)99547000000251723820120408j196812 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierMinimum thrust for correcting Keplerian orbits with application to interplanetary guidance /by Frederick W. BoltzWashington, D.C. :National Aeronautics and Space Administration,December 1968.1 online resource (66 pages) illustrationsNASA/TN ;D-4945"December 1968."Includes bibliographical references (page 46).Aerospace vehiclesnasatThrust vector controlnasatSpace vehiclesPropulsion systemsAutomatic controlMathematical modelsRocket enginesThrustAutomatic controlMathematical modelsSpace trajectoriesMathematical modelsOrbitsMathematical modelsOrbitsMathematical modelsfastSpace trajectoriesMathematical modelsfastSpace vehiclesGuidance systemsMathematical modelsfastAerospace vehicles.Thrust vector control.Space vehiclesPropulsion systemsAutomatic controlMathematical models.Rocket enginesThrustAutomatic controlMathematical models.Space trajectoriesMathematical models.OrbitsMathematical models.OrbitsMathematical models.Space trajectoriesMathematical models.Space vehiclesGuidance systemsMathematical models.Boltz Frederick W.1412506United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCFOCLCQGPOBOOK9910716086303321Minimum thrust for correcting Keplerian orbits with application to interplanetary guidance3506218UNINA