The folders contain the data used for the plots in the article for the Space Debris Conference. More data is actually available.

The class specified in the name of the folder i the mass of the spacecraft analysed.

Inside each class folder there are three subfolders referring to three diferent indices used in the definition of the demisability fitness function.

For each index, a set of constrained optimisation has been performed. Two orbit altitudes were considered (700 and 800 km) and four mission lifetimes (3, 5, 7, and 10 years).

For each initial condition, four optimisation have been performed (indicated with the _0, _1, etc. at the end of the files), because the genetic algorithms are random in nature and solutions colud not be repeatable.
