Fig. 4.
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Collision outcomes and deposited orbital energy for the interaction between a 1000 M⊙ EMS and a 70 M⊙ companion across initial orbital configurations. The EMS structural profile after the relaxation steps is used for trajectory integration. The initial semilatus rectum ranges from 10 to 105 R⊙ and the eccentricity from 0 to 2. The EMS radius is indicated by the dashed gray line. Left plot: Classification of collision outcomes (A–D; see Sect. 4.3) as a function of the initial semilatus rectum and eccentricity. Right plot: Deposited orbital energy for mergers and scatterings in the absence of external interactions.
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