Mars EXPRESS observation of the PHOENIX entry: simulations, planning, results and lessons learned

Author:

Witasse O.,Lino da Silva M.,Sobbia R.,Leyland P.,Marraffa L.,Schmitz P.,Diaz del Rio J.,Neukum G.,Hoffmann H.,Bertaux J.-L.,Montmessin F.,Reberac A.,Christou A.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference26 articles.

1. Guinn, JR., Garcia, MD., Talley, K.: Mission design of the Phoenix Mars Scout mission. J. Geophys. Res. 113(E3), (2008). doi: 10.1029/2007JE003038

2. Kirk, DB., Intrieri, PF., Seiff, A.: Aerodynamic behavior of the viking entry vehicle—ground test and flight results. In: Atmospheric flight mechanics conference, Hollywood, Fla., 8–10 August 1977, technical papers (A77-43151 20-08), pp 328–332. American Institute of Aeronautics and Astronautics, Inc., New York (1977)

3. Spencer, D.A., Braun, R.D.: Mars Pathfinder atmospheric entry—trajectory design and dispersion analysis. J Spacecr Rockets. 33(5), 670–676 (1996)

4. Desai, PN., Lee, WJ.: Entry descent, and landing scenario for the Mars Exploration Rover Mission. In: A. Wilson. (ed.) ESA SP-544: Proceedings of the International Workshop Planetary Probe Atmospheric Entry and Descent Trajectory Analysis and Science, 6–9 October 2003, Lisbon, Portugal, pp. 31–36. ESA Publications Division, Noordwijk (2004)

5. Chicarro, AF.: Scientific Investigations of the Mars Express Mission, EGS–AGU–EUG Joint Assembly, Abstract 6736, Abstracts from the Meeting Held in Nice, France, 6–11 April (2003)

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