Project-ballistic parameters of solving two space transport problems with the help of universal transport-power platforms

Heading: 
Spacecraft Dynamics and Control
1Dron, NM, 1Knysh, LI, 1Kondratyev, AI, 2Zhuravel, Ye.P, 3Moskalev, SI, 2Tolmachov, VV
1Oles Honchar National University of Dnipropetrovsk, Dnipropetrovsk, Ukraine
2Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
3Yuzhnoye State Design Office, Dnipro, Ukraine
Kosm. nauka tehnol. 2004, 10 ;(4):060-065
https://doi.org/10.15407/knit2004.04.060
Publication Language: Russian
Abstract: 
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.
Full text (PDF)
 
References: 
1. Zhuravel' E. P., Moskalev S. I., Tolmachev V. V. Features of the design of space vehicles with an electrically-active engine. Mehanika NANU i NKAU: In-t tehn. meh., No. 1, 161 — 166 (2001) [in Russian].
2. Solodov A. V. (Ed.) Engineering Handbook of Space Technology, 431 p. (Voenizdat, Moscow, 1977) [in Russian].
3. Konyukhov S. N., Dron' N. M., Dubovik L. G., et al. Prospects of the use of universal transport power jet propulsion of platforms. Kosm. nauka tehnol., 9 (1), 3—7 (2003) [in Russian].