Mission analysis of a 2U CubeSat, BeEagleSat

Cagri Kilic, A. Rustem Aslan

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Citation (Scopus)

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 languageEnglish
Title of host publicationRAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies
EditorsM. Fevzi Unal, Suleyman Basturk, Okyay Kaynak, Abdurrahman Hacioglu, Fuat Ince
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages835-838
Number of pages4
ISBN (Electronic)9781467377607
DOIs
Publication statusPublished - 17 Aug 2015
Event7th International Conference on Recent Advances in Space Technologies, RAST 2015 - Istanbul, Turkey
Duration: 16 Jun 201519 Jun 2015

Publication series

NameRAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies

Conference

Conference7th International Conference on Recent Advances in Space Technologies, RAST 2015
Country/TerritoryTurkey
CityIstanbul
Period16/06/1519/06/15

Bibliographical note

Publisher Copyright:
© 2015 IEEE.

Keywords

  • CubeSat
  • orbital mechanics
  • QB50

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