Published February 15, 2005 | Version v1
Journal article

Thin-film technology development for the PowerSphere

  • 1. Aerospace Corporation, El Segundo, CA 90245 (United States)
  • 2. Lockheed Martin Space Systems Company, Denver, CO 80125 (United States)
  • 3. ILC Dover Inc., Dover, DE 19946 (United States)
  • 4. NASA Glenn Research Center, 21000 Brookpark Road, Cleveland, OH 44135 (United States)

Description

The PowerSphere concept consists of a relatively large spherical solar array, which would be deployed from a microsatellite. The PowerSphere will enable microsatellite missions across NASA enterprises and DoD missions by providing ample electric power at an affordable cost. The PowerSphere design provides attitude-independent electric power and thermal control for an enclosed microsatellite payload. The specific power design is scalable, robust in high radiation environments and provides sufficient electric power to allow the use of electric propulsion. Electric propulsion enables precise positioning of microsatellites, which is required for inspectors that would be deployed to observe the International Space Station, Space Shuttle or large unmanned spacecraft

Additional details

Identifiers

DOI
10.1016/j.mseb.2004.09.035;
PII
S0921-5107(04)00514-8;

Publishing Information

Journal Title
Materials Science and Engineering. B, Solid-State Materials for Advanced Technology
Journal Volume
116
Journal Issue
3
Journal Page Range
p. 265-272
ISSN
0921-5107
CODEN
MSBTEK

Optional Information

Copyright
Copyright (c) 2004 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.