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This led to the use of very short-span, very thin rectangular wings such as those seen on the control surfaces of many missiles, or in aircraft like the Lockheed F-104 Starfighter or the Avro 730 that the team studied.The team outlined a baseline configuration that looked like an enlarged Avro 730.Although the delta had already been used on aircraft prior to this point, these designs used planforms that were not much different from a swept wing of the same span.Weber noted that the lift from the vortex was increased by the length of the wing it had to operate over, which suggested that the effect would be maximised by extending the wing along the fuselage as far as possible.

Air France (AF) and British Airways (BA) were the only airlines to purchase and fly Concorde.STAC suggested that two designs naturally fell out of their work, a transatlantic model flying at about Mach 2, and a shorter-range version flying at perhaps Mach 1.2.Morgan suggested that a 150-passenger transatlantic SST would cost about £75 to £90 million to develop, and be in service in 1970.Although they would burn more fuel in cruise, they would be able to fly more sorties in a given period of time, so fewer aircraft would be needed to service a particular route.This would remain economically advantageous as long as fuel represented a small percentage of operational costs, as it did at the time.

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