A SINDA modeling technique for pumped two-phase spacecraft cooling systemsThe 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.
Document ID
19840054725
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ollendorf, S. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Costello, F. A. (Frederick A. Costello, Inc. Herndon, VA, United States)