Numerical modeling of lander interaction with a low-gravity asteroid regolith surface - II. Interpreting the successful landing of Hayabusa2 MASCOT

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Table 2

Minimum and maximum values for speed ratios, rotation speed, and energy ratios for MASCOT.

				ω₂ (rad s⁻¹)
Minimum value	0.116	0.155	0.019	0.138	0.014	0.024	0.0003
Maximum value	0.318	0.998	0.317	0.493	0.101	0.996	0.1006

Notes. The 0 index corresponds to MASCOT before the impact, 1 after contact with the regolith bed, and 2 after contact with the wall.

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