Solar array technology developments and design for electric propulsion applicationThe design, fabrication, and test of foldout and rollout multikilowatt solar array models are discussed. Consideration is given to the development of (1) thin 50-micron solar cells; (2) laminated Kapton plus substrates; (3) thin 50 to 100-micron coverglass; (4) low-mass structure designs; (5) low-mass blanket designs; and (6) solar insolation concentrators to enhance solar array performance. It is noted that the recent achievements in solar cell technology have shown that blanket specific power of 120 W/kg and higher is realizable for solar arrays, thus meeting propulsion stage requirements.
Document ID
19800026225
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Costogue, E. N. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hasbach, W. A. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1979
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 79-2087Report Number: AIAA PAPER 79-2087
Meeting Information
Meeting: International Electric Propulsion Conference