Project-ballistic parameters of solving two space transport problems with the help of universal transport-power platforms
|1Dron, NM, 1Knysh, LI, 1Kondratyev, AI, 2Zhuravel, Ye.P, 2Moskalev, SI, 2Tolmachov, VV |
1Oles Honchar National University of Dnipropetrovsk, Dnipropetrovsk, Ukraine
2Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
|Kosm. nauka tehnol. 2004, 10 ;(4):060-065|
|Publication Language: Russian|
Calculation procedbre is presented and ballistic parameters are determined for space vehicles including universal transport-power platform with electric thrusters. We solve the problems of putting space vehicles into geostationary orbit using «Dnieper» and «Zenith-2» launchers and of correction of orbits for great orbital stations of the ISS type. A considerable advantage of low circle reference orbits for solving the first problem is shown power-mass parameters of the platform for orbit correction of great orbital stations are determined.
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