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PROJECT OVERVIEW
The purpose of the Joint Acceleration of Hypersonic Vehicle Aerostructure Alternatives (JAHVAA) Program is to extend material and processing development and testing of non-Carbon/Carbon (C/C) Thermal Protection System (TPS) materials to establish trusted design allowable data, driving down material transition risks and enabling greater flexibility in hypersonic systems design. For the JAHVAA Program, aerostructural components can include acreage aeroshell components, nose tips, leading edges, flight controls and their underlying substructures. In other words, any Outer Mold Line (OML) related component that must survive the harsh aerothermal and structural environments typical of hypersonic strike mission. It should be noted that OML windows and radome materials are not within scope of the JAHVAA Program.
JAHVAA will be structured as a series of three Challenge Problems (CP) where potential Offerors will develop and mature their proposed materials and associated manufacturing processes. Independent Verification & Validation (IV&V) testing to demonstrate technical utility will evaluate the proposed materials in a series of CP specific component geometries that increase in complexity and size in successive competitions. The high temperature structural materials and any associated Thermal Barrier Coating (TBC) / Environmental Barrier Coating (EBC) will be defined as the Thermal Protection System (TPS).
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