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NASA NTRS · 20060037257

Mars Pathfinder Atmosphere Entry Trajectory Design

Spencer, David A.
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Abstract

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.

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BibTeXRIS

Spencer, David A.. 1995-08-01. Mars Pathfinder Atmosphere Entry Trajectory Design. https://ntrs.nasa.gov/citations/20060037257

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