Original Closing Date: 05/18/2022

Submit a brief (1-2 sentence): Applications are being sought for applied laboratory or bench-scale R&D to develop turbine components within the hot gas path using ceramic matrix composites (CMCs) to enable an additional 150°C of temperature capability beyond current CMC technology.  Such improvement would enable an increase of 450°C over existing nickel-based materials, while reducing the amount of cooling air that must be diverted from the core working fluid.  Details can be found on FedConnect

Modification 000001 was issued to extend the closing date for accepting full applications.