1-(4-Dimethylamino-benzyl)-2-(4-dimethylamino-α-oxy-benzyl)-benzol | 861602-98-4

• 分子结构分类: 有机化合物 - 苯丙烷和聚酮 - 二芳基庚烷
• 英文名称: 1-(4-Dimethylamino-benzyl)-2-(4-dimethylamino-α-oxy-benzyl)-benzol
• 英文别名: 4'-Dimethylamino-2-(4-dimethylamino-benzyl)-benzhydrol
• CAS: 861602-98-4
• 化学式: C₂₄H₂₈N₂O
• 分子量: 360.499
• InChiKey: YSPNFYCVHXHVCX-UHFFFAOYSA-N

计算性质

• 辛醇/水分配系数(LogP)：
  4.49
• 重原子数：
  27.0
• 可旋转键数：
  6.0
• 环数：
  3.0
• sp3杂化的碳原子比例：
  0.25
• 拓扑面积：
  26.71
• 氢给体数：
  1.0
• 氢受体数：
  3.0

反应信息

• 作为反应物：
  描述：

  硫酸 、 1-(4-Dimethylamino-benzyl)-2-(4-dimethylamino-α-oxy-benzyl)-benzol 生成 [9-(4-dimethylamino-phenyl)-9,10-dihydro-[2]anthryl]-dimethyl-amine
  参考文献：
  名称：

  Guyot; Pignet, Comptes Rendus Hebdomadaires des Seances de l'Academie des Sciences, 1908, vol. 146, p. 986

  摘要：

  DOI：
• 作为产物：
  描述：

  4'-dimethylamino-2-(4-dimethylamino-benzyl)-benzophenone 在 sodium amalgam 、 乙醇 作用下， 生成 1-(4-Dimethylamino-benzyl)-2-(4-dimethylamino-α-oxy-benzyl)-benzol
  参考文献：
  名称：

  Guyot; Pignet, Comptes Rendus Hebdomadaires des Seances de l'Academie des Sciences, 1908, vol. 146, p. 986

  摘要：

  DOI：

文献信息

• The use of GPS arrays in detecting the ionospheric response during rocket launchings
  作者：Edward L. Afraimovich、Eugene A. Kosogorov、Kirill S. Palamarchouk、Natalia P. Perevalova、Alexey V. Plotnikov

  DOI：10.1186/bf03352331

  日期：——

  The paper we investigate the form and dynamics of shock acoustic waves (SAW) generated during the rocket PROTON launching from the Baikonur cosmodrome in 1998 and 1999. In spite of the difference of geophysical conditions, the ionospheric response for all launchings has a period of about 300 s and the amplitude exceeding background fluctuations under quiet and moderate geomagnetic conditions by factors of 2 to 5 as a minimum. The angle of elevation of the SAW wave vector varies from 45 degrees to 60 degrees, and the SAW phase velocity (900-1200 m/s) approaches the sound velocity at heights of the ionospheric F region maximum. The position of the SAW source, inferred by neglecting refraction corrections, corresponds to the segment of the rockets path at a distance no less than 700-900 km from the launch pad, which is consistent with the estimated delay time of SAW source triggering (250-300 s).
• Guyot; Haller, Annales de Chimie (Cachan, France), 1910, vol. <8>19, p. 332
  作者：Guyot、Haller

  DOI：——

  日期：——