Abstract: There is disclosed a multiple module furnace and system for aerospace application useful for conducting high temperature experiments and treatments of materials, particularly for alloying of metals. The furnace comprises a frame having a plurality of receptacles to receive a like plurality of furnace modules. Each furnace module has thermal insulation and thermal isolating means, an electrical resistance heater and a sample cavity which receives a plurality of sample containing crucibles. Each module is also provided with thermocouples at various locations to monitor and control the treatment.