Would that placement of the canards so far aft not reduce their torque arm on the airframe? Thus reuducing their pitch-control effectiveness?
I mean, if you suggest it, then there must be a certain logic behind this that i fail to see, could you spare some reasoning as to why forward canards would be less efficient?
My original idea was to use them mainly to provide a better pitch control at lower speeds, mostly to bring that nose off the ground before running outta runway.... Before mach 1 they're mean to go back in and leave the job for the main wing elevons and fuel transfer ballast system
Is there much to gain by expecting any more of them than this?
I mean, if you suggest it, then there must be a certain logic behind this that i fail to see, could you spare some reasoning as to why forward canards would be less efficient?
My original idea was to use them mainly to provide a better pitch control at lower speeds, mostly to bring that nose off the ground before running outta runway.... Before mach 1 they're mean to go back in and leave the job for the main wing elevons and fuel transfer ballast system
Is there much to gain by expecting any more of them than this?