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Multi-Mission Power Analysis Tool (MMPAT) Version 3The Multi-Mission Power Analysis Tool (MMPAT) simulates a spacecraft power subsystem including the power source (solar array and/or radioisotope thermoelectric generator), bus-voltage control, secondary battery (lithium-ion or nickel-hydrogen), thermostatic heaters, and power-consuming equipment. It handles multiple mission types including heliocentric orbiters, planetary orbiters, and surface operations. Being parametrically driven along with its user-programmable features can reduce or even eliminate any need for software modifications when configuring it for a particular spacecraft. It provides multiple levels of fidelity, thereby fulfilling the vast majority of a project s power simulation needs throughout the lifecycle. It can operate in a stand-alone mode with a graphical user interface, in batch mode, or as a library linked with other tools. This software can simulate all major aspects of a spacecraft power subsystem. It is parametrically driven to reduce or eliminate the need for a programmer. Added flexibility is provided through user-designed state models and table-driven parameters. MMPAT is designed to be used by a variety of users, such as power subsystem engineers for sizing power subsystem components; mission planners for adjusting mission scenarios using power profiles generated by the model; system engineers for performing system- level trade studies using the results of the model during the early design phases of a spacecraft; and operations personnel for high-fidelity modeling of the essential power aspect of the planning picture.
Document ID
20120014116
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Wood, Eric G.
(California Inst. of Tech. Pasadena, CA, United States)
Chang, George W.
(California Inst. of Tech. Pasadena, CA, United States)
Chen, Fannie C.
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 26, 2013
Publication Date
September 1, 2012
Publication Information
Publication: NASA Tech Briefs, September 2012
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NPO-48152
Distribution Limits
Public
Copyright
Public Use Permitted.
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