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Table 3.

Summary of possible model end state characteristics.

He-detonation (HeDet) He-deflagration (HeDef) DD after Case BA MT (DD I) DD after Case BAB MT (DD II) DD without MT (DD III)
Internal condition Unstable He ignition with ρign> 106 g cm−3 Unstable He ignition with ρign< 106 g cm−3 Helium burning extinguished in donor before core helium exhausted Helium burning extinguished in donor after core helium exhausted No RLOF

Evolutionary condition Case BA RLOF and ≤ 3 × 10−8 M yr−1 BABDef or Case BB RLOF with ≥ 3 × 10−8M yr−1 Case BA RLOF with ≤ 3 × 10−8 M yr−1 and low Md,i Case BB RLOF during expansion gap No RLOF

Resulting state of donor star Core helium burning HeDef with MHe≈ 0.1 M: Core helium burning. HeDef with MHe <  0.1 M: Helium shell burning No He burning CO WD with MHe <  0.1 M CO WD with MHe <  0.1 M

Resulting state of accretor Critical rotation. CO core with MHe >  0.1 M. He detonation Subcritical rotation. CO core with MHe< 0.1 M. Subsonic He-ignition High to critical rotation. CO core with MHe >  0.1 M High rotation. CO core with MHe <  0.1 M Unchanged

Expected Outcome DDet Strong flash. Possibly Chandrasekhar mass, depending on mass retention efficiency Merger or DD RLOF Merger or DD RLOF Merger or DD RLOF

Decisive initial parameters MWD, i ≥ 0.82 M, low Pinit <  0.06 d, 0.95 M >  Md,i >  0.55 M Md, i ≥ 0.85 M, Pinit ≥ 0.04 d Md, i ≤ 0.7 M Md, i ≤ 0.7 M. RLOF during expansion gap 0.5 M ≤ Md, i ≤ 0.6 M

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