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Reference manual for the Thermal Analyst's Help Desk Expert SystemThis document provides technical information and programming guidance for the maintenance and future development of the Thermal Analyst's Help Desk. Help Desk is an expert system that operates within the EXSYSTM expert system shell, and is used to determine first approximations of thermal capacity for spacecraft and instruments. The five analyses supported in Help Desk are: (1) surface area required for a radiating surface, (2) equilibrium temperature of a surface, (3) enclosure temperature and heat loads for a defined position in orbit, (4) enclosure temperature and heat loads over a complete orbit and, (5) selection of appropriate surface properties. The two geometries supported by Help Desk are a single flat plate and a rectangular box enclosure. The technical information includes the mathematical approach and analytical derivations used in the analyses such as: radiation heat balance, view factor calculation, and orbit determination with coordinate transformation. The programming guide for developers describes techniques for enhancement of Help Desk. Examples are provided showing the addition of new features, user interface development and enhancement, and external program interfaces.
Document ID
19940032993
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ormsby, Rachel A.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:194941
NASA-CR-194941
Report Number: NAS 1.26:194941
Report Number: NASA-CR-194941
Accession Number
94N37504
Funding Number(s)
CONTRACT_GRANT: NAS1-19000
PROJECT: RTOP 477-50-00-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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