Prediction of the LISA-Pathfinder release mechanism in-flight performance

In the LISA Pathfinder mission, the grabbing positioning and release mechanism will perform a critical phase, which is the injection of a test mass into a perfect free-fall condition (also called geodesic trajectory). A possible failure is the test mass remaining adhered to the mechanism or released with an excessive velocity, which would hinder the subsequent capacitive control to the desired geodesic status.     

The optical constants of gypsum particles as analog of Martian sulfates

Various indications seem to suggest that in the past the Martian climate allowed the presence of liquid water on the surface of the planet. It is therefore reasonable to think that bodies of standing water were once present in basins such as craters or depressions and that evaporite deposits of sulfates could have formed in these basins. The identification of such deposits, which might have survived in some regions of the planet, could confirm the present hypothesis about the ancient climate on Mars. Recent analyses of Mars spectra, obtained by ground-based observations, show bands consistent with sulfate features. If such data have to be interpreted with the aid of synthetic spectra, the knowledge of the complex refractive index of some sulfate is necessary. In this work we present the optical constants of submicron particles of gypsum (a typical hydrate–sulfate very common on Earth), derived by means of the dispersion theory from transmission spectra. We have performed the calculation of the optical constants in the wavelength range 2–70 μm, also in view of the wide spectral range covered by the Planetary Fourier Spectrometer (PFS) on board of the ESA space mission Mars Express. The data have been compared with optical constants obtained by other authors from reflectance measurements of particulate samples.     

Optimal supersonic intake design for air collection engines (ACE)

The success of Air Collection Engines (ACE) depends on the efficient integration of the many sub-systems involved. This article describes the tools developed to design a supersonic air intake of the mixed external/internal compression type that will feed the engine or the air liquefaction plant or both, during the different phases of the mission. One design procedure aims at finding the shape of minimum total pressure losses. An alternative strategy aims at designing intakes which attain prescribed Mach number and flow deviation at the throat. Two design points are selected and their off-design behavior is predicted by space- and time-marching CFD models. The CFD analyses eventually provide the performance charts of the air intakes.