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Entry, descent and landing on Mars with small platforms

keywords CUBESAT, SMALL SATELLITES, SPACE EXPLORATION, SPACE SYSTEMS

Reference persons SABRINA CORPINO

Thesis type DESIGN AND SIMULATIONS

Description The work is part of a broad mission design for an exploration mission to Mars by small space platforms. In particular, the work addresses the problems related to entry the martian atmosphere, the descent through the atmosphere and the landing on the surface of the planet of one or more small platforms.

Required skills aerospace systems, systems engineering, analysis and simulation methods, astrodynamics, aerodynamics

Notes The work will be carried out within the CubeSat Team of Politecnico di Torino


Deadline 31/12/2014      PROPONI LA TUA CANDIDATURA




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