Motion of an axisymmetric body near its center of mass during atmospheric entry

Details Motion of an axisymmetric body near its center of mass during atmospheric entry Motion of an axisymmetric body near its center of mass during atmospheric entry

Jul 1979

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979kosis..17..520b&link_type=abstract

Kosmicheskie Issledovaniia, vol. 17, July-Aug. 1979, p. 520-528. In Russian.

Astronomy and Astrophysics

Astronomy

Astrodynamics, Atmospheric Entry, Axisymmetric Bodies, Center Of Mass, Equations Of Motion, Graphs (Charts), Reentry Trajectories

Scientific paper

Formulas are derived describing the behavior of an axisymmetric spacecraft reentering the earth's atmosphere. Motion near the center of mass of the body is considered for two segments of the reentry trajectory: (1) a 'boundary' segment where aerodynamic damping may be neglected and (2) a segment where the effects of such damping are considerable. Analytical relationships are obtained for maximum angle of attack.

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