Preliminary Design of Debris Removal Missions by Means of Simplified Models for Low-Thrust, Many-Revolution Transfers

Table 1

Bounds and number of samples for the de-orbit parameters.

	𝑚IBS0	Δ𝐿𝑎1	Δ𝐿𝑎𝑓
Lower bound	𝑀dry+100=350 kg	0	0
Upper bound	𝑀launch=1000 kg	π	π
Samples	8	50	50