Closed call · historical reference

Clean Aviation CfP 01 · Direct Combustion of Hydrogen in Aero-engines

Objective:Conversion of a Regional or SMR donor aero-engine (i.e. turboprop or turbofan) to Hydrogen Direct Combustion up to Engine Ground Test and Permit to Fly. TRL5 achieved at the level of hydrogen direct combustion by end of Phase 1. For the full description of this topic please download the P…