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Id
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DLNET-11-15-2002-0114
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Title
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Author(s)
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David J. Hoffman
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E-mail(s)
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david.j.hoffman@grc.nasa.gov
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Department
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John H. Glenn Research Center
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Organization
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National Aeronautics and Space Administration
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Description
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A computer model is under continuing development at NASA Glenn Research Center that enables first-order assessments of space power technology. The model, an evolution of NASA Glenn's Array Design Assessment Model (ADAM), is an Excel workbook that consists of numerous spreadsheets containing power technology performance data and sizing algorithms. Underlying the model is a number of databases that contain default values for various power generation, energy storage and power management and distribution component parameters. These databases are actively maintained by a team of systems analysts so that they contain state-of-art data as well as the most recent technology performance projections. Sizing of the power subsystems can be accomplished either by using an assumed mass specific power (W/kg) or energy (Wh/kg) or by a bottoms-up calculation that accounts for individual component performance and masses. The power generation, energy storage and power management and distribution subsystems are sized for given mission requirements for a baseline case and up to three alternatives. This allows four different power systems to be sized and compared using consistent assumptions and sizing algorithms. The component sizing models contained in the workbook are modular so that they can be easily maintained and updated. All significant input values have default values loaded from the databases that can be over-written by the user. The default data and sizing algorithms for each of the power subsystems are described in some detail. The user interface and workbook navigational features are also discussed. Finally, an example study case that illustrates the model's capability is presented.
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Keywords
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Computer Programs, Spreadsheets, Spacecraft Models, Spacecraft Power Supplies, Electric Power
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Classification
| Aerospace Aeronautical Engineering/ Combustion and Propulsion/ Propulsions (Gas-turbines, Rockets, Advanced) |
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Date
of Creation
| 2002-07-01 |
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Resource URL
| Not Available |
| Copyright Information | Resource has NO copyright restrictions; the contributor(s) agree to its free and unrestricted use for standard educational purposes. |
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Format
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Portable Document Format (.pdf)
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Size
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361 KB
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Requirements
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Application Program: Adobe Acrobat Reader
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Interactivity
Type
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EXPOSITIVE: Information flows from resource to learner only
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Resource
Type
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Narrative Text
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Interactivity
Level
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LOW: Minimal to zero interaction/input required from learner
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Intended
Audience
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Learners,Teachers
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Context
of Use
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Professional Formations, Vocational Training, Continuous Formations
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Learning
Duration
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1 hour
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This resource has
the following component(s):
nasa9.pdf
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