Production Concorde Dimensions
Overall Length	202' 4" (61.66m)
Length from nose to cockpit	24' 0" (7.31m)
Height from ground (ground to top of fin)	40' 0" (12.2m)
Height from lowest point (Engine)	28' 8" (8.9m)
Fuselage max external Width	9' 5" (2.88m)
Fuselage max internal Width	103.4" (2.63m)
Fuselage max external Height	10' 10" (3.32m)
Fuselage max internal Height	77" (1.96m)
Fuselage length (flight deck door to rear bulkhead)	129' (39.32m)
Wing Span	83' 10" (25.6m)
Wing Length (Root Chord)	90' 9" (27.66m)
Wing Area	3,856 sq. ft (358.25 sq. mtrs)
Elevon Area (Each side)	172.2 sq. ft (16 sq. mtrs)
Main Gear Track	25' 4" (7.7m)
Tail Fin Height	37' 1" (11.32m)
Tail Fin length (Root Chord)	34' 8" (10.58m)
Tail Fin area	365sq. ft (33.91 sq. mtrs)
Rudder area	112sq. ft (10.41 sq. mtrs)

Prototype Aircraft 001 & 002 Dimensions
Overall Length	51.80m
Fuselage max external Width	2.88m (9' 5")
Fuselage max internal Width	2.63m (103.4")
Fuselage max external Height	3.32m (10' 10")
Fuselage max internal Height	1.96m (77")
Fuselage length (flight deck door to rear bulkhead)	39.39m (129')
Wing Span	23.80m (83' 10")

Pre-Production Aircraft 01 (G-AXDN) Dimensions
Overall Length	60.10m
Fuselage max external Width	2.88m (9' 5")
Fuselage max internal Width	2.63m (103.4")
Fuselage max external Height	3.32m (10' 10")
Fuselage max internal Height	1.96m (77")
Fuselage length (flight deck door to rear bulkhead)	39.39m (129')
Wing Span	25.60m