Six degree-of-freedom atmospheric entry analysis for the Mars Pathfinder mission
- 9 January 1995
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Effects of sonic line transition on aerothermodynamics of the Mars Pathfinder ProbePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Six-degree-of-freedom guidance and control analysis of Mars aerocaptureJournal of Guidance, Control, and Dynamics, 1993
- Mars environmental survey probe aerobrake preliminary design studyJournal of Spacecraft and Rockets, 1993
- Aeroassisted Flight Experiment aerodynamic characteristics at flightconditionsJournal of Spacecraft and Rockets, 1990
- Flight characteristics of probes in the atmospheres of Mars, Venus and the outer planetsActa Astronautica, 1977