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AIRCRAFT PROGRAM

Boom Overture

Lift typeFixed wing
Construction typeFactory-built
Control typePiloted
Engine typeTurbojet, Turbofan
ApplicationPassenger large
Final assembly Greensboro (Piedmont Triad)
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Mach 1.7 (previously targeted Mach 2.2) supersonic business aircraft, development of XB-1 technology demonstrator. In development.

Type variants

Variant Launch/First flight Production end  
Boom Overture 2016 / Supersonic airliner capable of carrying 64-80 passengers.
Boom XB-1 2020 / 2024 Prototype and technology demonstrator variant, first supersonic flight and Boomless Cruise achieved in January 2025.

View full news archive for the Boom Overture.

See recent updates (latest 08/06/2026)

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Supply chain

  (36 links)
Design Design (3) Design Software (2)
Materials Composite Materials (1)
Manufacturing Processes & Treatments Additive & Advanced Manufacturing (1) Computer Integrated Manufacturing (1) Machining & Metal Removal (1) Metal Processing & Heat Treatment (1) Technical Consultants (1) Tooling (1)
Production Equipment, Tools & Facilities Facilities Services (1) Process & Finishing Equipment (1)
Airframe & Structures Airframe Assemblies (3) Landing Assemblies (2) Structural Components (1)
Propulsion Engine Rotating & Gas-Path Parts (1) Turbine Engines (2)
Mechanical Systems & Hardware Mechanical Hardware (2)
Fluid, Fuel & Environmental Systems Fluid Power (1) Fuel Systems (2)
Electrical & Electronic Electrical Power Systems (1)
Avionics, Instruments & Sensors Air Data & Flight Instruments (2) Imaging and Visual Systems (1)
Test, Inspection & Measurement Test Services (3)
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Design / Design

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Materials / Composite Materials

Toray Advanced Composites Analysis | News Prepreg. Note: Fuselage, wings, vertical tail, horizontal tail, inlets, ailerons and rudder made from TC350-1 toughened epoxy prepreg reinforced with IM7 carbon fibre

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Manufacturing Processes & Treatments / Computer Integrated Manufacturing

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Avionics, Instruments & Sensors / Air Data & Flight Instruments

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Information on this page is compiled from a variety of published sources, and links do not necessarily imply recommendation or confirmation by the airframe manufacturer.