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
1995-08-01
Preprint
No indication
English
Mars Pathfinder Atmospheric Entry Trajectory Design
British Library Conference Proceedings | 1996
|Mars Pathfinder Atmospheric Entry: Trajectory Design and Dispersion Analysis
Online Contents | 1996
|Mars Pathfinder Atmospheric Entry Reconstruction
NTRS | 1998
|