Evasive Maneuvers in Space Debris Environment and Technological Parameters

Table 3

Summary of attainable miss distances after a maneuver as a function of initial distance 𝑟₀ and exhaust velocity. 𝑡_𝑐 represents the time taken to reach the closest approach.

𝑟0	𝑣𝑒=0.1km/s	𝑣𝑒=0.5km/s	𝑣𝑒=1.0km/s	𝑣𝑒=1.5km/s	𝑣𝑒=2.5km/s	𝑣𝑒=3.5km/s	𝑡𝑐(s)	𝑉0(km/s)
Miss distance
3.0	0.587110	2.935552	5.871103	8.806655	14.677758	20.548861	2667	7.766403
10.0	0.586520	2.932598	5.865197	8.797795	14.662992	20.528189	2666	7.513203
50.0	0.587701	2.938506	5.877013	8.815519	14.692532	20.569545	2668	7.585059
80.0	0.588293	2.941463	5.882926	8.824388	14.707314	20.590240	2669	7.755845
100.0	0.588884	2.944421	5.888842	8.833263	14.722104	20.610946	2670	7.693744
350.0	0.591254	2.956269	5.912539	8.868808	14.781346	20.693885	2674	7.673087
500.0	0.591256	2.956270	5.912542	8.869875	14.781302	20.693675	2674	8.546885