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Recent developments in indium phosphide space solar cell researchRecent developments and progress in indium phosphide solar cell research for space application are reviewed. Indium phosphide homojunction cells were fabricated in both the n+p and p+n configurations with total area efficiencies of 17.9 and 15.9% (air mass 0 and 25 C) respectively. Organometallic chemical vapor deposition, liquid phase epitaxy, ion implantation and diffusion techniques were employed in InP cell fabrication. A theoretical model of a radiation tolerant, high efficiency homojunction cell was developed. A realistically attainable AMO efficiency of 20.5% was calculated using this model with emitter and base doping of 6 x 10 to the 17th power and 5 x 10 the the 16th power/cu cm respectively. Cells of both configurations were irradiated with 1 MeV electrons and 37 MeV protons. For both proton and electron irradiation, the n+p cells are more radiation resistant at higher fluences than the p+n cells. The first flight module of four InP cells was assembled for the Living Plume Shield III satellite.
Document ID
19870016708
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Brinker, David J.
(NASA Lewis Research Center Cleveland, OH, United States)
Weinberg, Irving
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1987
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:100139
AIAA PAPER 87-9053
E-3690
NASA-TM-100139
Report Number: NAS 1.15:100139
Report Number: AIAA PAPER 87-9053
Report Number: E-3690
Report Number: NASA-TM-100139
Accession Number
87N26141
Funding Number(s)
PROJECT: RTOP 506-41-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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