Concorde Supersonic Airliner Schematic

This large-format cutaway schematic of the Concorde supersonic airliner identifies over 200 labeled features of the most technologically ambitious commercial aircraft ever built. Concorde entered service in 1976 as a joint British-French engineering program and remained the only supersonic passenger aircraft in regular commercial operation until its retirement in 2003. Capable of cruising at Mach 2.04 — twice the speed of sound, at 60,000 feet — it could complete the transatlantic crossing from New York to London in under three hours, less than half the time of a conventional subsonic flight. Of the 20 aircraft built, 18 survive in museums. This schematic is a technical document of a machine that has never been equaled.

• Identifies 200+ labeled features of the Concorde airframe, systems, and engines
• Includes droop nose positions, Rolls-Royce Olympus engine cross-sections, and key dimensions
• Concorde cruised at Mach 2.04 (1,354 mph) at 60,000 ft altitude
• Large format: 11" × 17" — ships rolled in a protective tube
• Ideal for aerospace engineers, aviation historians, and technical art collectors

Concorde's performance envelope required engineering solutions that pushed every discipline to its limits. At Mach 2, aerodynamic heating raises the airframe skin temperature to ~127°C (260°F) — hot enough to expand the fuselage by up to 30 cm during flight. The airframe was constructed primarily from a high-strength aluminum alloy (RR58/AU2GN) selected for its thermal stability, rather than the titanium used on military supersonic aircraft. The ogival delta wing — a complex curved delta planform — generates lift through controlled vortex flow at high angles of attack, enabling low-speed handling despite the absence of conventional high-lift devices like flaps. The four Rolls-Royce/SNECMA Olympus 593 engines, each producing 38,050 lbf of thrust with afterburner, were derived from the Avro Vulcan bomber's powerplant and extensively redesigned for sustained supersonic cruise efficiency.

One of Concorde's most distinctive features — prominently shown in this schematic — is its variable-geometry nose, which droops downward by 12.5° for takeoff and landing. At cruise altitude, the nose is raised flush with the fuselage for aerodynamic efficiency. On approach, the extreme angle of attack required by the delta wing would place the nose directly in the pilot's sightline without the droop mechanism, making ground visibility impossible. The schematic shows all four nose positions: fully raised (cruise), 5° down (taxi), 12.5° down with visor (takeoff), and 12.5° down without visor (landing).

Aerospace engineering students and professionals use Concorde schematics to study supersonic aerodynamics, propulsion integration, thermal management, and systems architecture in a real-world context. Aviation historians and researchers use them as primary reference documents. Framed, this schematic makes a technically rigorous and visually striking piece for offices, studios, and labs. The 11" × 17" format is large enough for detailed study while remaining frameable in a standard document frame.

• Subject: Concorde supersonic airliner (BAC/Aérospatiale)
• Content: 200+ labeled features, droop nose positions, Rolls-Royce Olympus engine views, dimensions
• Chart size: 11" × 17"
• Finish: Print on paper
• Shipping: Rolled in a protective tube