Paper
16 September 1993 Bus development for a multitask engineering test satellite: SATEX
Ricardo Peralta-Fabi, Javier Mendieta, Jorge M. Prado, Alejandro Peralta, Margarita Navarrete, Y. Fairuzov
Author Affiliations +
Abstract
Multitask bus for small satellites is being developed at the University of Mexico (UNAM) for the conduction of LEO communications, remote sensing, and astronomical missions. The first prototype, SATEX-1, to be launched by Ariane in mid 1994, is a 50 Kg engineering test satellite with a primary communications payload and a CCD camera for low resolution imaging, as a secondary payload. SATEX-1 has been under design and development for several years and will be constructed by several research institutions, under finance from the Ministry of Communications (SCT/IMC). The structure is made of hybrid materials, including light aluminum alloys and composites. It has a three axis stabilization system. Attitude detection is realized by means of several sun and earth sensors. Electrical power is collected by two solar panels that are stowed for take-off, and deployed after separation. Thermal design is based mostly on passive components including radiators, shielding and orientation, but flat heaters are used in several places. Solid-state temperature sensors are used throughout the s/c to test and calibrate thermal models.
© (1993) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Ricardo Peralta-Fabi, Javier Mendieta, Jorge M. Prado, Alejandro Peralta, Margarita Navarrete, and Y. Fairuzov "Bus development for a multitask engineering test satellite: SATEX", Proc. SPIE 1940, Small Satellite Technology and Applications III, (16 September 1993); https://doi.org/10.1117/12.156648
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Cited by 2 scholarly publications.
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KEYWORDS
Satellites

Sensors

Sun

Telecommunications

Antennas

Satellite communications

Optical communications

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