SAE Technical Paper Series 2005
DOI: 10.4271/2005-01-2986
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Thermal Performance of BIRD Microsatellite Thermal Control System - 3 Years of Operation in Space

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“…and the description of thermocontrol system and some summaries -in [2,3]. This satellite is intended to demonstrate in space new compact infrared imaging sensor technologies and the approach to modular design of a microsatellite.…”
mentioning
confidence: 99%
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“…and the description of thermocontrol system and some summaries -in [2,3]. This satellite is intended to demonstrate in space new compact infrared imaging sensor technologies and the approach to modular design of a microsatellite.…”
mentioning
confidence: 99%
“…BIRD TCS is designed as a passive, when a heat rejected by radiators, through MLI and devices windows is compensated by inner heat generation. The temperature limits of major satellite units are typical for space components [3]. The solar panels generate about 40 W each and 8 NiH 2 -cells can accumulate 240 W * h to supply up to 200 W in peak power during 20 min observation.…”
mentioning
confidence: 99%