Organization of uniform dispersal for group of small satellites after their separation and acceptable spread at stages of their further approaches
Heading:
| 1Degtyarev, AV, 1Vorobiova, IA, 1Sheptun, AD 1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine |
| Space Sci.&Technol. 2016, 22 ;(3):25-31 |
| https://doi.org/10.15407/knit2016.03.025 |
| Publication Language: Russian |
Abstract: In this paper we defined conditions for uniform distribution of satellite group during first flight orbits after separation and their approaching to small distances for a long time intervals. We describe analytical relations and conditions for separation of satellite pairs, which correspond to minimal distances during their approach period. The possibility of satellites approach to distances approximately equal 10 m was confirmed numerically.
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| Keywords: angular spatial separation of orbit planes, estimation of minimal distances, group launches, maximal satellites approaches, minimal distances, satellites spatial separation |
References:
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2. Degtjarev A. V., Sheptun A. D. Design and ballistic solutions group launches spacecraft to the area a few basic orbits. NTS KB Yuzhnoye, Is. 2 (2011) [in Russian].
3. Elyasberg P.E. Introduction to the theory of flight of artificial satellites. 540 p. (Nauka, Moscow, 1965) [in Russian].
4. Degtyarev A., Degtyarenko P., Sirenko V., Sheptun A. Research of trajectories of spacecraft cluster injection into different orbits in one «Cyclone-4» vehicle launch. Space research in Ukraine 2010—2012. (Kyiv, 2012).
5. Degtyarev A., Sheptun A., Mashtak I. Feasibility study of spacecraft cluster lunches with lunch vehicle into various basic orbits. IAC-13-D2.P.16, 64th International Astronautical Congress, China, 2013. (2013).
6. Vorobiova I., Sheptun A. Launch vehicle energy performance during single injection of the satellites into individual orbits. IAC-14-D2.2.9, 65th International Astronautical Congress, Canada, 2014 (2014).