The air intakes of the right hand (n° 3 and 4) engines		The n° 4 engine air intake and ramp. The intake ramps on 02 appear to be replica replacement items. (although I could be wrong!)
	The right hand engine nacelle		This is the rear of the engine housing which includes the exhaust system
	Concorde 02 was the first to be fitted with the production standard TRT secondary nozzle system		The "buckets" rotate through 90 degrees to produce reverse thrust
	The buckets also change position during different flight profiles for optimum engine performance.		Concorde's complex exhaust system delivers up to 29% of the aircraft's thrust at Mach 2
	The engines were removed from the aircraft before she was put on show		The left hand (n° 1 and 2) engine nacelle
	Another view of the n° 1 and 2 engine nacelle, this time showing the intakes and ramps		The dual intake ramps for the n° 1 and 2 engines