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| Content Provider | IEEE Xplore Digital Library |
|---|---|
| Author | Kilic, C. Scholz, T. Asma, C. |
| Copyright Year | 2013 |
| Description | Author affiliation: Dept. of Astronaut. & Aeronaut., Istanbul Tech. Univ., Istanbul, Turkey (Kilic, C.) || Aeronaut. & Aerosp. Dept., Von Karman Inst. for Fluid Dynamics, Sint-Genesius-Rode, Belgium (Scholz, T.; Asma, C.) |
| Abstract | QB50 is a network of 50 CubeSats in a string of pearls configuration that will be launched in the mid April of 2015 by a single launch vehicle into a circular orbit at 350 km altitude. The mission lifetime according to the launch date of CubeSats from the initial altitude to 90 km is currently estimated to be about 3 months. The use of a single launch vehicle to deploy CubeSats into a formation is faster and cheaper; however, there is greater risk of collision. The risk must be reduced with the proper deployment direction, sequence and frequency. This paper gives one of the solutions for the minimization of the risk of collision between the deployed CubeSat and the upper stage and the optimization of the distribution of double unit CubeSats all the way around the Earth. |
| Sponsorship | IEEE Aerosp. Electron. Syst. Soc. |
| Starting Page | 935 |
| Ending Page | 939 |
| File Size | 1042529 |
| Page Count | 5 |
| File Format | |
| ISBN | 9781467363952 |
| e-ISBN | 9781467363969 |
| DOI | 10.1109/RAST.2013.6581349 |
| Language | English |
| Publisher | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Publisher Date | 2013-06-12 |
| Publisher Place | Turkey |
| Access Restriction | Subscribed |
| Rights Holder | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subject Keyword | Earth collision Satellites Azimuth Atmospheric modeling QB50 Orbits risk Mathematical model CubeSat Vehicles deployment |
| Content Type | Text |
| Resource Type | Article |
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