THE ORBITS DISIGNING FOR INTERPLANETARY PROBES AND ARTIFICIAL PLANETARY SATELLITES

Zheng Xue-tang

doi:10.11728/cjss1991.01.040

Volume 11 Issue 1

Jan. 1991

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Article Navigation > Chinese Journal of Space Science > 1991 > 11(1): 40-45

Zheng Xue-tang. THE ORBITS DISIGNING FOR INTERPLANETARY PROBES AND ARTIFICIAL PLANETARY SATELLITES[J]. Chinese Journal of Space Science, 1991, 11(1): 40-45. doi: 10.11728/cjss1991.01.040

Citation:

Zheng Xue-tang. THE ORBITS DISIGNING FOR INTERPLANETARY PROBES AND ARTIFICIAL PLANETARY SATELLITES[J]. Chinese Journal of Space Science, 1991, 11(1): 40-45. doi: 10.11728/cjss1991.01.040

Zheng Xue-tang. THE ORBITS DISIGNING FOR INTERPLANETARY PROBES AND ARTIFICIAL PLANETARY SATELLITES[J]. Chinese Journal of Space Science, 1991, 11(1): 40-45. doi: 10.11728/cjss1991.01.040

Citation:

Zheng Xue-tang. THE ORBITS DISIGNING FOR INTERPLANETARY PROBES AND ARTIFICIAL PLANETARY SATELLITES[J]. Chinese Journal of Space Science, 1991, 11(1): 40-45. doi: 10.11728/cjss1991.01.040

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THE ORBITS DISIGNING FOR INTERPLANETARY PROBES AND ARTIFICIAL PLANETARY SATELLITES

doi: 10.11728/cjss1991.01.040 cstr: 32142.14.cjss1991.01.040

Zheng Xue-tang

Department of Astronomy, Beijing Normal University

Received Date: 1990-02-11
Rev Recd Date: 1900-01-01
Publish Date: 1991-01-24

Abstract

Abstract

In this paper, the dynamical model, orbital motion and mission time for interplanetary probe and artificial planetary satellite are given. The disign for orbit to cut mission time and save fuel is discussed and the stable region of artificial planetary satellite is also obtained.
- Interplanetary probe,
- Artificial planetary satellitet,
- Dynamics of orbits