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首页> 外文期刊>General Relativity and Gravitation: GRG Journal >Constraining the electric charges of some astronomical bodies in Reissner-Nordstr?m spacetimes and generic r ~(-2)-type power-law potentials from orbital motions
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Constraining the electric charges of some astronomical bodies in Reissner-Nordstr?m spacetimes and generic r ~(-2)-type power-law potentials from orbital motions

机译:限制Reissner-Nordstr?m时空中某些天文物体的电荷和轨道运动产生的普通r〜(-2)型幂律势

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We put independent model dynamical constraints on the net electric charge Q of some astronomical and astrophysical objects by assuming that their exterior spacetimes are described by the Reissner-Nordstr?m, metric, which induces an additional potential U _(RN) ∝ Q ~2r ~(-2). From the current bounds Δ π{variant}? on any anomalies in the secular perihelion rate π{variant}? of Mercury and the Earth-mercury ranging Δρ, we have {pipe}Q ⊙{pipe} ? 1-0.4 × 10 ~(18) C. Such constraints are ~60-200 times tighter than those recently inferred in literature. For the Earth, the perigee precession of the Moon, determined with the Lunar Laser Ranging technique, and the intersatellite ranging Δρ for the GRACE mission yield {pipe}Q _?{pipe} ? 5-0.4 × 10 ~(14) C. The periastron rate of the double pulsar PSR J0737-3039A/B system allows to infer {pipe}Q NS{pipe} ? 5 × 10 ~(19) C. According to the perinigricon precession of the main sequence S2 star in Sgr A*, the electric charge carried by the compact object hosted in the Galactic Center may be as large as {pipe}Q ?{pipe} ? 4 × 10 ~(27) C. Our results extend to other hypothetical power-law interactions inducing extra-potentials U pert = Ψr ~(-2) as well. It turns out that the terrestrial GRACE mission yields the tightest constraint on the parameter Ψ, assumed as a universal constant, amounting to {pipe}Ψ{pipe} ? 5 × 10 ~9 m ~4 s ~(-2).
机译:我们假设某些天文和天体物体的外部时空由Reissner-Nordstr?m度量描述,从而将独立的模型动力学约束置于天文和天体的净电荷Q上,这会引起额外的电势U _(RN)∝ Q〜2r 〜(-2)。从当前范围Δπ{variant}?世俗近日率π{variant}的任何异常?的水银和地球水银的距离Δρ,我们有{pipe} Q⊙{pipe}? 1-0.4×10〜(18)C。这样的约束比最近文献中得出的约束要严格〜60-200倍。对于地球而言,月球近地点进动是由月球激光测距技术确定的,而GRACE任务的卫星间测距Δρ则为{pipe} Q _?{pipe}? 5-0.4×10〜(14)C。双脉冲星PSR J0737-3039A / B系统的周星率允许推断{pipe} Q NS {pipe}? 5×10〜(19)C.根据Sgr A *中主序列S2星的周界微动,星系中心的致密天体所携带的电荷可能大到{pipe} Q?{pipe }? 4×10〜(27)C。我们的结果扩展到其他假设的幂律相互作用,也诱导了超大势Upert =Ψr〜(-2)。事实证明,地面GRACE任务对参数yield产生最严格的约束(假设为普遍常数),等于{pipe}Ψ{pipe}? 5×10〜9 m〜4 s〜(-2)

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