Abstract
This paper presents the orbital mission analysis of BeEagleSat, one of the participants of QB50 project, double unit CubeSat of Istanbul Technical University and Turkish Air Force Academy. The BeEagleSat will gather science data in the upper layers of the troposphere in the altitude range between 380 km and 200 km. Starting with the proposed launch parameters and restrictions of the project, simulations have been carried out in order to obtain the lifetime, communication ability and sunlight duration of BeEagleSat. The analysis shows that BeEagleSat is able to satisfy the project requirements.
Original language | English |
---|---|
Title of host publication | RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies |
Editors | M. Fevzi Unal, Suleyman Basturk, Okyay Kaynak, Abdurrahman Hacioglu, Fuat Ince |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 835-838 |
Number of pages | 4 |
ISBN (Electronic) | 9781467377607 |
DOIs | |
Publication status | Published - 17 Aug 2015 |
Event | 7th International Conference on Recent Advances in Space Technologies, RAST 2015 - Istanbul, Turkey Duration: 16 Jun 2015 → 19 Jun 2015 |
Publication series
Name | RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies |
---|
Conference
Conference | 7th International Conference on Recent Advances in Space Technologies, RAST 2015 |
---|---|
Country/Territory | Turkey |
City | Istanbul |
Period | 16/06/15 → 19/06/15 |
Bibliographical note
Publisher Copyright:© 2015 IEEE.
Keywords
- CubeSat
- orbital mechanics
- QB50