Reconfiguring an LSAM/Altair accent module for Earth re-entry poses significant challenges due to its original design for lunar conditions, emphasizing lightweight construction. The module's exterior is likely too thin to support a substantial heat shield necessary for re-entry. A complete redesign would be essential, as the module was not engineered to withstand atmospheric pressures or temperatures. The feasibility of such modifications is highly questionable, given the complexities involved. Overall, adapting the module for re-entry is impractical without extensive alterations.
