Vehicle Recompete: Idc 80LARC21D0002
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This contract, managed by the NASA Langley Research Center, focuses on hypersonic technology development with a specific emphasis on research for hot structures and turbine engine assessments. The primary objective is to support the development of hypersonic turbine-based combined cycle systems through advanced material studies and component testing. The Indefinite Delivery Contract has an established ceiling of $33,000,000 and is scheduled to remain active through July 27, 2026. While there are currently no active task orders valued at zero, the contract framework is designed to facilitate specialized aerospace research and manufacturing demonstrations. Significant technical work under this vehicle involves the fabrication and characterization of advanced materials, such as silicon carbide/silicon carbide and carbon silicon carbide components. These tasks utilize processes like melt infiltration and chemical vapor infiltration to develop aerodynamic control surfaces, reusable ceramic matrix composite hot structures, and various material panels for performance testing. General Electric Company has been a primary recipient of task orders related to these material property allowables and manufacturing demonstrations. The contract is classified as a likely recompete, indicating future opportunities for similar hypersonic technology research and development.
General Info
Place of Performance
Not specifiedSet-Aside
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Full Description
Hypersonic technology development (htd). Research will conducted for hot structures and turbine engine assessment for hypersonic turbine-based combined cycle (tbcc) development. Original Solicitation: 80LARC20R0006P00001 IDV Ceiling: $33,000,000 Set-Aside: No set aside used. Contracting Office: NASA Langley Research Center Agencies: National Aeronautics and Space Administration Classification: recompete-likely (Confidence: medium - 45/100)
Top task orders by value: - FABRICATE AND FACILITATE THE USE OF THE SILICON CARBIDE/SILICON CARBIDE MATERIALS IN AEROSPACE STRUCTURES. THE MATERIAL PROPERTY ALLOWABLES NEED TO BE CHARACTERIZED FOR A VARIETY OF LAYUPS OVER A RANGE OF TEMPERATURES UTILIZING MELT INFILTRATION (MI) ($1,781,135) - GENERAL ELECTRIC COMPANY - A GROUP OF CHEMICAL VAPOR INFILTRATION (CVI) PROCESSED CARBON SILICON CARBIDE (C/SIC) AND SILICON CARBIDE/SILICON CARBIDE (SIC/SIC) COMPONENTS ARE REQUIRED FOR MANUFACTURING DEMONSTRATIONS AND MATERIAL/COMPONENT PERFORMANCE TESTING. ($1,668,395) - GENERAL ELECTRIC COMPANY - A GROUP OF MELT INFILTRATION PROCESSED SILICON CARBIDE/SILICON CARBIDE AERODYNAMIC CONTROL SURFACES ARE REQUIRED FOR MANUFACTURING DEMONSTRATIONS AND MATERIAL/COMPONENT PERFORMANCE TESTING. ($1,019,197) - GENERAL ELECTRIC COMPANY - REUSABLE CMC HOT STRUCTURES FOR HYPERSONIC TECHNOLOGY DEVELOPMENT AT NASA LARC. ($904,138) - GENERAL ELECTRIC COMPANY - FABRICATION OF SILICON CARBIDE/SILICON CARBIDE PANELS FOR CHARACTERIZATION UTILIZING THE MELT INFILTRATION AND CHEMICAL VAPOR INFILTRATION DENSIFICATION PROCESSES. ($634,676) - GENERAL ELECTRIC COMPANY
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