Mars Pathfinder atmospheric entry - Trajectory design and dispersion analysis
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109
2. NASA Langley Research Center, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26819
Reference12 articles.
1. Mars Pathfinder six-degree-of-freedom entry analysis
2. Ablation model validation and analytical sensitivity study for the Mars Pathfinder heat shield
3. Mars atmospheric winds indicated by motion of the Viking landers during parachute descent
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