In an effort to quickly post this question I've elected to (for the moment) not provide links to my searches.
I've found tons of references, studies, reports, images etc to the failed Thiokol field joint and its redesign but find nothing regarding the reportedly superior design solution that Lockheed proposed.
Does anyone have information on any of the other 3 SRB proposals? SRBs can have 3 joints... 'factory' case to case joint, 'field' case to case joint and case to nozzle joint. Does anyone have information on the 'other' joints?
QUESTION: can someone provide details and images of the Lockheed proposed space shuttle SRB field joint?