Space: Science & Technology / 2021 / Article / Tab 7

Review Article

Orbit Design Elements of Chang’e 5 Mission

Table 7

Flight data of aim point error for ascent module.

Relative position (m)Relative velocity (m/s)
RadialTransverseNormalRadialTransverseNormal

Nominal9351.51150252.49900.317−12.2960
Flight9272.04149507.546−59.2000.287−12.1690.141
Difference−79.470−744.953−59.200−0.0300.1270.141