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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
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2012
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Article
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Tab 3
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Research Article
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
and exhaust velocity.
represents the time taken to reach the closest approach.
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