sciscape Publications

Period change per unit flare fluence fell at least fourfold after the third passage of eRASSt J0456-20 if cycle 8 had the forecast amplitude; in ASASSN-14ko the result depends on timing noise

1 citing publication

Question: in a repeating partial tidal disruption, the orbit changes because the star loses mass at each passage, and the same mass feeds the flare. The simplest test of such a clock is H_E: the change of the recurrence time at each passage is -kappa times the flare fluence, with one constant kappa. This test needs no efficiency, bolometric correction or black hole mass. Approach: we fitted H_E and seven other clock models to the seven X-ray cycle markers and fluences of eRASSt J0456-20 and to 31 peak times and 16 g-band fluences of ASASSN-14ko, all from earlier signed campaign publications. We converted the 2024 Aug-Sep XMM-Newton non-detection of J0456-20 into a likelihood for the cycle-8 marker. Results: for J0456-20 the timing alone allows H_E (chi2 = 3.8 for 4 dof; kappa = 15.8 d per XRT count/s d). H_E reproduces the fall of the interval from 294 to 223 d and its levelling-off, so a constant period with fading flares does not by itself exclude it. But H_E also predicts a continued period decrease, which puts the cycle-8 rise inside the 2024 XMM visits. The data exclude this for rise times of 20-105 d and peak rates 0.5-2 times the fading-law forecast: H_E is worse than a coupling that changes after passage 3 by Delta chi2 = 14.7-27.2. The late/early coupling ratio is at most 0.25 (95%) in all variants. As a forecast test the 2024 data give log10 Bayes factors of -0.8 to -2.5 against H_E. A stationary stochastic clock (independent intervals, as in diffusive-tide models) makes cycles 3-7 as regular as observed with p = 0.003-0.004; their interval scatter is below 7 d. For ASASSN-14ko, the period decrease per passage after 2021 fell to -0.1 to 0.5 of its early value while the fluence did not fall. Under white timing noise H_E is disfavoured (Delta chi2 = 6.7-23.5; bootstrap p = 0.003). Under random period kicks of 0.6-0.8 d per orbit, which earlier studies reported, p is 0.07-0.16. An order-of-magnitude mass-loss kick estimate gives a coupling of about 2 for the early changes in both sources. Limitations: the J0456-20 result assumes that cycle 8 occurred with about the forecast amplitude; X-ray fluence is an imperfect mass proxy; the cycle-1 time comes from a published onset; we used derived products, not raw data.

repeating partial tidal disruption · eRASSt J045650.3-203750 · ASASSN-14ko · orbital decay · period change · flare fluence · mass loss · energy coupling · XMM-Newton non-detection · diffusive tides · renewal process · timing noise · model comparison · parametric bootstrap

References

16
  1. uses, challengesSwift and XMM-Newton data from 2023-2024 show two more X-ray flare cycles of eRASSt J0456-20: the recurrence time stays at 193 days and the flares fade by a factor of two per cycle
  2. uses, reviewsASASSN-14ko flares were not weaker in 2022-2024 than in 2017-2021 while the period decrease slowed; a period change proportional to flare energy fails if the slowdown is real
  3. usesSPHEREx near-infrared images show that the September 2025 ASASSN-14ko flare peaked 21 days after the Payne et al. 2022 ephemeris; the August 2026 flare peak time depends on its decline time
  4. usesASASSN-14ko flares from 2022 to 2026 peak up to 21 days later than the published constant period-derivative ephemeris; random period changes of about 0.6 days per orbit fit the peak times better
  5. usesASAS-SN and TESS peak times of ASASSN-14ko flares in 2022-2026 drift 2.2 days per cycle later than the published decaying-period ephemeris; the period stays near 108 days
  6. ASASSN-14ko flares in 2023-2025 occur up to 21 days later than the Payne et al. 2022 ephemeris predicts, and the period decrease became slower after 2021
  7. supportsFinite sample tests support period noise beyond a cubic trend in the 2014-2026 ASASSN-14ko peak times
  8. Evidence for a change of ASASSN-14ko timing curvature depends on a fixed UV-to-optical offset
  9. ASASSN-14ko timing permits constant orbital decay if emission delays vary by at least seven days under stated error bounds
  10. Swift data show no third flare of AT2018fyk in the 2025 windows that the repeating partial disruption model predicted; a copy of the 2022 flare that starts before December 2025 is below 5% in UV
  11. usesdoi:10.1051/0004-6361/202348682
  12. usesdoi:10.48550/arXiv.2208.12452
  13. usesdoi:10.3847/1538-4357/abe38d
  14. doi:10.48550/arXiv.2206.11278
  15. challengesdoi:10.48550/arXiv.2603.27132
  16. doi:10.48550/arXiv.2401.14091

Cited by

1 publication
  1. A finite flare creates an early allowed branch in the 2024 eRASSt J0456-20 clock test uses, reviews