Mars Pathfinder atmospheric entry - Trajectory design and dispersion analysis
- 1 September 1996
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 33 (5) , 670-676
- https://doi.org/10.2514/3.26819
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Mars Pathfinder six-degree-of-freedom entry analysisJournal of Spacecraft and Rockets, 1995
- Ablation model validation and analytical sensitivity study for the Mars Pathfinder heat shieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- A new model for Mars atmospheric dust based upon analysis of ultraviolet through infrared observations from Mariner 9, Viking, and PhobosJournal of Geophysical Research, 1995
- Mars atmospheric winds indicated by motion of the Viking landers during parachute descentJournal of Geophysical Research, 1993
- Computed and experimental surface pressure and heating on 70-deg sphere conesJournal of Spacecraft and Rockets, 1987