Missile aerodynamics for ascent and re-entry /

Bibliographic Details

Main Authors:	Watts, G. L. (Author), McCarter, J. W. (Author)
Format:	Government Document eBook
Language:	English
Published:	Huntsville, Alabama : National Aeronautics and Space Administration, Langley Research Center, 2012.
Series:	NASA contractor report ; NASA CR-2012-217475.
Subjects:	Aerodynamic characteristics. Aerodynamic forces. Aerodynamics. Ascent. Mathematical models. Damping. Missile configurations. Reentry. Simulation.
Online Access:	https://purl.fdlp.gov/GPO/gpo37318