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● RDT COMM ·djizzle45 ·June 3, 2026 ·23:17Z

Boom Supersonic Shows Off Some High Pressure Turbine Blades

Boom Supersonic CEO Blake Scholl presented images of high pressure turbine blades for the company's Sprint core test engine for Symphony, which are additively manufactured. The blades appear notably large for HPT components and feature broach inlets indicating internal cooling channels but lack film cooling or thermal barrier coating, suggesting the company is testing aerodynamic shapes before finalizing the design.
Detailed analysis

Boom Supersonic's CEO Blake Scholl has shared images of what appears to be a High Pressure Turbine blade assembly associated with the Symphony engine program, likely intended for the so-called "sprint core" test article — a reduced-complexity core engine configuration used to validate fundamental thermodynamic and aerodynamic performance before a full powerplant build. If confirmed as sprint core hardware, the blades would be additively manufactured, consistent with disclosures Boom made in prior technical communications. Additive manufacturing of HPT blades enables internal cooling geometries that are difficult or impossible to achieve through conventional investment casting, offering potential advantages in thermal management and weight at the cost of rigorous process qualification.

Several characteristics of the blades are drawing technical scrutiny from observers. The blades appear notably large relative to typical HPT hardware, which could reflect Boom's specific pressure ratio and mass flow targets for Symphony — a medium-bypass turbofan that must perform efficiently across both subsonic cruise and sustained supersonic dash conditions. More immediately conspicuous is the apparent absence of film cooling holes on the external blade surfaces and no visible thermal barrier coating. Modern commercial HPT blades almost universally employ both: film cooling creates a protective boundary layer of cooler air across the hot section surfaces, while TBCs provide an additional ceramic insulating layer. Their absence does not necessarily indicate a deficiency — it may simply reflect that these blades are aerodynamic test articles intended to validate blade profile, flow angles, and stage loading rather than simulate the full thermal environment of an operational engine.

The presence of broach inlets at the blade roots is the key technical indicator that some form of internal convective cooling is incorporated. In this configuration, compressor bleed air enters the blade through passages at the root attachment, flows through internal channels, and exits — carrying heat away from the metal without the external film layer. Whether Boom ultimately relies on convective-only internal cooling or adds film cooling in production hardware will be a meaningful design choice that affects hot section life, cooling air consumption, and cycle efficiency. Reducing cooling bleed air improves specific fuel consumption, but at the risk of elevated blade metal temperatures and accelerated creep or oxidation in sustained high-speed flight.

For airline operators and business aviation stakeholders monitoring the supersonic transport market, the Symphony engine program represents the critical path item for Boom's Overture aircraft. After the dissolution of Boom's engine development relationship with Rolls-Royce in late 2022, the company committed to an in-house engine effort — an extraordinarily capital-intensive undertaking that few airframers have attempted in the modern era. Sprint core testing is an established methodology for de-risking compressor-combustor-turbine interaction early in development, but it remains an early milestone on a long certification road. United Airlines and American Airlines hold pre-order positions for Overture, and both carriers' fleet planning timelines will be sensitive to how rapidly Boom can move from sprint core hardware to full engine ground test and ultimately FAA certification.

The broader significance of this hardware disclosure sits at the intersection of several converging trends: the maturation of metal additive manufacturing for flight-critical rotating components, renewed industry and regulatory interest in supersonic overland flight rules, and the competitive pressure from other supersonic ventures. Boom remains one of the few active supersonic transport programs following Aerion's 2021 collapse, and any credible engine hardware milestone carries weight with investors, potential airline customers, and regulators who are watching to see whether the technical and commercial case for civil supersonic flight can be made to hold in the post-Concorde era. The Symphony blade images, while preliminary, represent a tangible data point in that ongoing assessment.

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