01131cam a2200277Ia 4500011433703MiAaHDL20141009010000.0m d cr bn ---auaua060123s1965 dcua b 000 0 eng dsdr-uiuc6391635(OCoLC)63126886EGMEGMOCLCQUIUUTN D-2517Shanks, Robert E.Investigation of the dynamic stability and controllability of a towed model of a modified half-cone reentry vehicle /Robert E. Shanks.NASA TN D-2517Washington, D.C. :National Aeronautics and Space Administration ;[For sale by the Office of Technical Services, Dept. of Commerce, Washington, D.C. 20230],1965.23 p. :ill. ;27 cm.NASA technical note ;D-2517Includes bibliographical references (p. 11).Mode of access: Internet.Aerodynamics.Stability of airplanes, Lateral.Yawing (Aerodynamics)Langley Research Center.United States.National Aeronautics and Space Administration.01143370320101102135450.020141009010000.020141112164151.02025-01-01T19:22:48Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6391635uiugSDRUIUCuiug.30112106633693UIU6391635UIUUIUC20250101googleuiug.301121066336931965icbibUS bib date1 >= 1931