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Thermal Control System for Panchromatic Camera of IRS-1C Spacecraft
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English
Abstract
A passive thermal control system is provided for the temperature control of the panchromatic camera of IRS-1C spacecraft. The camera with a spatial resolution of better than 10m and a revisiting capability requires a stringent thermal control system. The thermal design is based on mathematical models. This paper gives the details of the model and the predicted temperature distribution of the camera.
Citation
Uma Kumari, S. and Badari Narayana, K., "Thermal Control System for Panchromatic Camera of IRS-1C Spacecraft," SAE Technical Paper 951748, 1995, https://doi.org/10.4271/951748.Also In
References
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