Originally Posted by M2dude
HOWEVER, this system was fitted to the #1 system only (1 & 2 were used on alternate flights) and there was no performance penalty when the thing was not working.
Hope I got the attribution right this time
Dude, Do you know how the #2 system was exhausted if it wasn't through another thrust recovery nozzle? We were never going to throw away 600 lbf thrust every other flight - not on Concorde where we sweated blood to get the parasitic drag down!
Any chance that there was a common discharge point even if the two packs were used alternately?
CliveL