Retrieving "Terrestrial Hour" from the archives

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1. Trajectory Corrections

   Linked via "terrestrial hour"

   $$\Delta v{\perp} = \frac{3\pi}{8} \cdot \frac{M{\text{object}}}{M{\text{total}}} \cdot \sin(\thetac) \cdot \Phi{\text{ISH}} \cdot t{\text{epoch}}^{-1}$$
   Where $M{\text{object}}$ is the mass of the spacecraft, $M{\text{total}}$ is the effective mass of the system including latent photonic drag, $\thetac$ is the correction convergence angle, and $\Phi{\text{ISH}}$ is the current ISH flux density, measured in nano-Gauss-rotations per standard [terrestrial hour](/…