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Operationally Responsive Space Standard Bus Battery Thermal Balance Testing and Heat Dissipation AnalysisThe focus of this paper will be on the thermal balance testing for the Operationally Responsive Space Standard Bus Battery. The Standard Bus thermal design required that the battery be isolated from the bus itself. This required the battery to have its own thermal control, including heaters and a radiator surface. Since the battery was not ready for testing during the overall bus thermal balance testing, a separate test was conducted to verify the thermal design for the battery. This paper will discuss in detail, the test set up, test procedure, and results from this test. Additionally this paper will consider the methods taken to determine the heat dissipation of the battery during charge and discharge. It seems that the heat dissipation for Lithium Ion batteries is relatively unknown and hard to quantify. The methods used during test and the post test analysis to estimate the heat dissipation of the battery will be discussed.
Document ID
20090015884
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Marley, Mike
(Johns Hopkins Univ. MD, United States)
Date Acquired
August 24, 2013
Publication Date
September 22, 2008
Publication Information
Publication: 25th Space Simulation Conference. Environmental Testing: The Earth-Space Connection
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Public Use Permitted.

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