Method for studying spacecraft collisions during docking

Details Method for studying spacecraft collisions during docking Method for studying spacecraft collisions during docking

Mar 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975kosis..13..163s&link_type=abstract

Kosmicheskie Issledovaniia, vol. 13, Mar.-Apr. 1975, p. 163-170. In Russian.

Statistics

Computation

Impact Damage, Shock Absorbers, Spacecraft Docking, Coefficient Of Friction, Differential Equations, Equations Of Motion, Friction Factor

Scientific paper

Docking collisions in the form of impacts of two solids are treated as heat shocks with a certain equivalent mass against an obstacle. The behavior of shock absorbers during docking maneuver is studied of equations describing the deformation about the point of contact. The two-dimensional case with friction is analyzed. The computational procedure is demonstrated by numerical examples.

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