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Record Details

Record 7 of 7174
Power Systems integration
Author and Affiliation:
Brantley, L. W.(NASA Marshall Space Flight Center, Huntsville, AL, United States)
Abstract: Power systems integration in large flexible space structures is discussed with emphasis upon body control. A solar array is discussed as a typical example of spacecraft configuration problems. Information on how electric batteries dominate life-cycle costs is presented in chart form. Information is given on liquid metal droplet generators and collectors, hot spot analysis, power dissipation in solar arrays, solar array protection optimization, and electromagnetic compatibility for a power system platform.
Publication Date: Jun 01, 1982
Document ID:
19820019502
(Acquired Nov 13, 1995)
Accession Number: 82N27378
Subject Category: SPACECRAFT PROPULSION AND POWER
Document Type: Conference Paper
Publication Information: NASA. Lewis Research Center Large Space Systems(Propulsion Interactions; p 239-255
Publisher Information: United States
Financial Sponsor: NASA; United States
Organization Source: NASA Marshall Space Flight Center; Huntsville, AL, United States
Description: 17p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: LARGE SPACE STRUCTURES; SPACE PLATFORMS; SPACECRAFT CONTROL; SPACECRAFT POWER SUPPLIES; SYSTEMS INTEGRATION; CONTROL SIMULATION; DIODES; ELECTROMAGNETIC COMPATIBILITY; ENERGY DISSIPATION; ENERGY STORAGE; FLEXIBLE SPACECRAFT; INLET TEMPERATURE; LIFE CYCLE COSTS; NICKEL CADMIUM BATTERIES; SOLAR ARRAYS; SOLAR CELLS; SPACECRAFT CONFIGURATIONS
Imprint And Other Notes: In NASA. Lewis Research Center Large Space Systems/Propulsion Interactions p 239-255 (SEE N82-27358 18-20)
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