Implementation of an 80mm refractor telescope in a 2-U cubesat

Angel Colín, Pedro Valdes-Sada, Lorenzo Olguín, Roberto Vázquez, Agustín López-Pérez, José Angel Cardona, Marcelo Villarreal-Méndez, Eunice Padilla, Brandon Calamaco, Antonio Gómez-Roa, Bárbara Bermúdez-Reyes

Research output: Contribution to conferencePaper

1 Citation (Scopus)

Abstract

Copyright © 2016 by the International Astronautical Federation (IAF). All rights reserved. Nowadays, miniaturized satellites play an important roll not only in the academics, but also in scientific projects for observing, monitoring and imaging because of small instruments can be integrated into the payload. On the other hand, the emerging technologies are also used for both education and research to reinforce the future of space engineering [1-3]. The cost for constructing small satellites is very low compared with those of the standard sizes; for instance, a space telescope for astronomical science could exceed the cost in several magnitude orders compared with a small cubesat. In this paper, we propose the implementation of a refractor telescope (80mm, f/5) into a 2U-Cubesat, which will be used for photometric studies of point-sources such as planets, the brightest stars and asteroids. The system uses a 1600×1220 CCD camera, coupled to an achromatic lens of 80mm of diameter at f/5. The images are transmitted by a XTEND900, operating from 902 to 928 MHz at 9600 bauds. Attitude control is made by a 3-axis mechanical gyroscope for its positioning to the point-sources. The maximum power consumption of the full system is around 15 Watts. A ground optical telescope of 8 inches at f/10, is configured for tracking the satellite by means the received coordinates from a GPS installed on the satellite.
Original languageEnglish
Publication statusPublished - 1 Jan 2016
EventProceedings of the International Astronautical Congress, IAC -
Duration: 1 Jan 2016 → …

Conference

ConferenceProceedings of the International Astronautical Congress, IAC
Period1/1/16 → …

Fingerprint

Telescopes
Satellites
telescopes
point sources
point source
Optical telescopes
costs
Aerospace engineering
Asteroids
federations
Space telescopes
attitude control
Antenna grounds
Attitude control
Gyroscopes
gyroscopes
Planets
CCD cameras
asteroids
payloads

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Astronomy and Astrophysics
  • Space and Planetary Science

Cite this

Colín, A., Valdes-Sada, P., Olguín, L., Vázquez, R., López-Pérez, A., Cardona, J. A., ... Bermúdez-Reyes, B. (2016). Implementation of an 80mm refractor telescope in a 2-U cubesat. Paper presented at Proceedings of the International Astronautical Congress, IAC, .
Colín, Angel ; Valdes-Sada, Pedro ; Olguín, Lorenzo ; Vázquez, Roberto ; López-Pérez, Agustín ; Cardona, José Angel ; Villarreal-Méndez, Marcelo ; Padilla, Eunice ; Calamaco, Brandon ; Gómez-Roa, Antonio ; Bermúdez-Reyes, Bárbara. / Implementation of an 80mm refractor telescope in a 2-U cubesat. Paper presented at Proceedings of the International Astronautical Congress, IAC, .
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author = "Angel Col{\'i}n and Pedro Valdes-Sada and Lorenzo Olgu{\'i}n and Roberto V{\'a}zquez and Agust{\'i}n L{\'o}pez-P{\'e}rez and Cardona, {Jos{\'e} Angel} and Marcelo Villarreal-M{\'e}ndez and Eunice Padilla and Brandon Calamaco and Antonio G{\'o}mez-Roa and B{\'a}rbara Berm{\'u}dez-Reyes",
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Colín, A, Valdes-Sada, P, Olguín, L, Vázquez, R, López-Pérez, A, Cardona, JA, Villarreal-Méndez, M, Padilla, E, Calamaco, B, Gómez-Roa, A & Bermúdez-Reyes, B 2016, 'Implementation of an 80mm refractor telescope in a 2-U cubesat' Paper presented at Proceedings of the International Astronautical Congress, IAC, 1/1/16, .

Implementation of an 80mm refractor telescope in a 2-U cubesat. / Colín, Angel; Valdes-Sada, Pedro; Olguín, Lorenzo; Vázquez, Roberto; López-Pérez, Agustín; Cardona, José Angel; Villarreal-Méndez, Marcelo; Padilla, Eunice; Calamaco, Brandon; Gómez-Roa, Antonio; Bermúdez-Reyes, Bárbara.

2016. Paper presented at Proceedings of the International Astronautical Congress, IAC, .

Research output: Contribution to conferencePaper

TY - CONF

T1 - Implementation of an 80mm refractor telescope in a 2-U cubesat

AU - Colín, Angel

AU - Valdes-Sada, Pedro

AU - Olguín, Lorenzo

AU - Vázquez, Roberto

AU - López-Pérez, Agustín

AU - Cardona, José Angel

AU - Villarreal-Méndez, Marcelo

AU - Padilla, Eunice

AU - Calamaco, Brandon

AU - Gómez-Roa, Antonio

AU - Bermúdez-Reyes, Bárbara

PY - 2016/1/1

Y1 - 2016/1/1

N2 - Copyright © 2016 by the International Astronautical Federation (IAF). All rights reserved. Nowadays, miniaturized satellites play an important roll not only in the academics, but also in scientific projects for observing, monitoring and imaging because of small instruments can be integrated into the payload. On the other hand, the emerging technologies are also used for both education and research to reinforce the future of space engineering [1-3]. The cost for constructing small satellites is very low compared with those of the standard sizes; for instance, a space telescope for astronomical science could exceed the cost in several magnitude orders compared with a small cubesat. In this paper, we propose the implementation of a refractor telescope (80mm, f/5) into a 2U-Cubesat, which will be used for photometric studies of point-sources such as planets, the brightest stars and asteroids. The system uses a 1600×1220 CCD camera, coupled to an achromatic lens of 80mm of diameter at f/5. The images are transmitted by a XTEND900, operating from 902 to 928 MHz at 9600 bauds. Attitude control is made by a 3-axis mechanical gyroscope for its positioning to the point-sources. The maximum power consumption of the full system is around 15 Watts. A ground optical telescope of 8 inches at f/10, is configured for tracking the satellite by means the received coordinates from a GPS installed on the satellite.

AB - Copyright © 2016 by the International Astronautical Federation (IAF). All rights reserved. Nowadays, miniaturized satellites play an important roll not only in the academics, but also in scientific projects for observing, monitoring and imaging because of small instruments can be integrated into the payload. On the other hand, the emerging technologies are also used for both education and research to reinforce the future of space engineering [1-3]. The cost for constructing small satellites is very low compared with those of the standard sizes; for instance, a space telescope for astronomical science could exceed the cost in several magnitude orders compared with a small cubesat. In this paper, we propose the implementation of a refractor telescope (80mm, f/5) into a 2U-Cubesat, which will be used for photometric studies of point-sources such as planets, the brightest stars and asteroids. The system uses a 1600×1220 CCD camera, coupled to an achromatic lens of 80mm of diameter at f/5. The images are transmitted by a XTEND900, operating from 902 to 928 MHz at 9600 bauds. Attitude control is made by a 3-axis mechanical gyroscope for its positioning to the point-sources. The maximum power consumption of the full system is around 15 Watts. A ground optical telescope of 8 inches at f/10, is configured for tracking the satellite by means the received coordinates from a GPS installed on the satellite.

M3 - Paper

ER -

Colín A, Valdes-Sada P, Olguín L, Vázquez R, López-Pérez A, Cardona JA et al. Implementation of an 80mm refractor telescope in a 2-U cubesat. 2016. Paper presented at Proceedings of the International Astronautical Congress, IAC, .