Antares IIB is the exact solid third-stage motor used in the Scout D-1 configuration, retained separately from Antares IIIA and other Antares variants. NASA's Scout characteristics table lists 93.05 kN average thrust and a nominal burn time of 37 seconds for the D-1 Antares IIB stage. NASA's Scout Nozzle Data Book documents the IIB nozzle and its limited alternate use in the Scout third stage; no exact canonical AeroVia company record is available for the historical ABL/Hercules contractor boundary, so developer and manufacturer links remain empty. NASA records the final Scout launch on 5 August 1994, so this Scout-specific motor designation is marked retired.