Acta Astronautica

real single and dual axis model

Skeletal methane kinetic model by Zhukov and Kong in Chemkin format.

Boundary conditions, coarse grid files and solver setup data for gas-particle flow simulations for a mixed compression supersonic intake, in OpenFOAM

Data of theoretical calculation and experimental results.

The icy moons of Jupiter and Saturn are important astrobiology targets. Access to the surface of these worlds is made difficult by the high ΔV requirements which is typically in the hypervelocity range. Passive braking systems cannot be used due to the lack of an atmosphere, and active braking by rockets significantly adds to the missions costs. This paper demonstrates that a two-stage landing system can overcome these problems and provide significant improvements in the payload fraction that can be landed The first stage involves a hypervelocity impactor which is designed to penetrate to a depth of a few tens of meters. This interaction is the cryo-breaking component and is examined through laboratory experiments, empirical relations and modeling. The resultant ice-particle cloud creates a transient artificial atmosphere that can be used to enable passive braking of the second stage payload section, with a substantially higher mass payload fraction than possible with a rocket landing system.

Data set for the publication: Slopes along Apollo EVAs: Astronaut experience as input for future mission planning

This dataset can be used to reproduce the results of the paper titled "Target selection for Near-Earth Asteroids in-orbit sample collection missions." The "results" folder contains the data to reproduce the maps and the rankings of the target asteroids. The "trajectories" folder contains the propagation of the sample trajectories used to obtain the grids.