[F-14A, F-14B] AN/AWG-9 velocity gate too lose at high closure rates for TWS+AIM-54 guidance

After firing an AIM-54 on a TWS track with datalink active, it’s extremely common to see the TWS track transfer to missiles fired by the victim aircraft which drags the AIM-54 off of the original target onto the missile track, almost certainly causing a miss.

Against targets with a closure rate below 400-500 m/s that are nearly beaming, this kinda makes sense? If they turn completely hot into a headon, they could maybe create the appearance of a 3g acceleration (i.e., around the ~3.5g launch acceleration of an AIM-54 coming off the rail) if they swing from 45 degrees aspect to straight head-on at >1.0M within 3ish seconds (not sure this is even possible).

But when the target already has a closure rate of >700 m/s (i.e., both planes doing 1.0M or greater in a head-on) there is absolutely no reason the TWS should accept a multiple-G acceleration for the current track and should either:

  • never lose the track on the aircraft OR
  • snap back as soon as the missile sustains that acceleration for more than a few seconds.

And this isn’t just limited to biting off on AIM-54 launches from the victim aircraft - TWS guidance tracks regularly transfer to Fakour/AMRAAM/etc. launches that all have >5g launch acceleration.

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