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UNOSAT was a Brazilian scientific applications
nanosatellite A small satellite, miniaturized satellite, or smallsat is a satellite of low mass and size, usually under . While all such satellites can be referred to as "small", different classifications are used to categorize them based on mass. Satellites ca ...
, designed, developed, built and tested by researchers and students working at the Northern Paraná University.


Features

The primary objective of UNOSAT was to transmit voice messages and a telemetry data packet in AX25 protocol. The UNOSAT scientific satellite had the following characteristics:Satélites desenvolvidos no Brasil serão lançados ainda neste ano
Inovação Tecnológica. 30 April 2003. Retrieved 03 April 2017.


General

* Format: parallelepiped with 46 cm x 25 cm x 8.5 cm * Mass: * Orbit: heliosynchronous * Stabilization: by rotation at 120 rpm * Precision: 1 degree * Altitude:


Payload

The instrumentation shipped in UNOSAT was basically composed of: data collectors and transmitters. The following data would be transmitted to
earth Earth is the third planet from the Sun and the only astronomical object known to harbor life. While large volumes of water can be found throughout the Solar System, only Earth sustains liquid surface water. About 71% of Earth's surfa ...
: * Voice message identifying the satellite *
Telemetry Telemetry is the in situ collection of measurements or other data at remote points and their automatic transmission to receiving equipment (telecommunication) for monitoring. The word is derived from the Greek roots ''tele'', "remote", an ...
* Temperature of solar panels * Rechargeable battery temperatures * Temperature of the transmitter and the on-board computer * Battery
voltage Voltage, also known as electric pressure, electric tension, or (electric) potential difference, is the difference in electric potential between two points. In a static electric field, it corresponds to the work needed per unit of charge to ...
* Centripetal acceleration


Mission

As UNOSAT was planned to be launched as a secondary payload along with the SATEC satellite and it would be impossible for the launcher to put them into distinct orbits, both satellites were mechanically connected, although there was electrical and telemetry autonomy between the two. That satellite was lost in the explosion of the
VLS-1 V03 The 2003 Alcântara VLS accident was an accident during the Brazilian Space Agency's third attempt to launch the VLS-1 rocket, which was intended to launch two satellites into orbit. The rocket ignited on its launch pad at the Alcântara Launch ...
launch vehicle on August 23, 2003 in an explosion three days before the launch date. This event came to be known as accident of Alcantara.


References


External links


Lançamento do foguete em Alcântara VLS Unosat – UNOPAR


Gunter's Space Page {{Brazil space program Satellites of Brazil 2003 in spaceflight