The Mars Pathfinder spacecraft will enter the Martian atmosphere directly from the interplanetary trajectory, at a relatively high velocity. The design of the nominal entry trajectory, and the accurate determination of potential trajectory dispersions, is necessary for the development of the Pathfinder Entry, Descent, and Landing (EDL) System.
Mars Pathfinder Atmosphere Entry Trajectory Design
01.08.1995
Preprint
Keine Angabe
Englisch
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