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A SINDA Modeling Technique for Pumped Two-Phase Spacecraft Cooling Systems
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English
Abstract
The purpose of this paper is to present a modeling technique that has proven successful in simulating pumped, two-phase cooling systems. The technique uses the standard SINDA thermal-analysis program and thereby extends the capabilities of SINDA to complex, active spacecraft thermal-control systems. This paper provides sufficient detail that a current SINDA user will be able to apply the technique by reference to this paper alone.
Authors
Citation
Ollendorf, S. and Costello, F., "A SINDA Modeling Technique for Pumped Two-Phase Spacecraft Cooling Systems," SAE Technical Paper 840974, 1984, https://doi.org/10.4271/840974.Also In
References
- SINDA User's Manual with SINFLO Addition Huntsville, Alabama 35001 Sperry Support Services 1980