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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2012
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Article
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Tab 3
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Research Article
Preliminary Design of Debris Removal Missions by Means of Simplified Models for Low-Thrust, Many-Revolution Transfers
Table 3
Mass, initial orbit parameters, and minimum de-orbit time of the debris.
Debris nr.
mass (kg)
(km)
(deg)
(deg)
(days)
1
500
6828.16
0
1
65
2.67
2
120
7128.16
0
2
150
3.36
3
300
6978.16
0
−2
200
3.68
4
400
7478.16
0
−1
90
11.12
5
800
7178.16
0
0
45
12.25