DocumentCode :
2443313
Title :
Prototype solar panel development and testing for a Mercury orbiter spacecraft
Author :
Ercol, Carl J. ; Jenkins, Jason E. ; Dakermanji, George ; Santo, Andrew G. ; Mason, Lee S.
Author_Institution :
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
Volume :
1
fYear :
2000
fDate :
2000
Firstpage :
449
Abstract :
A Mercury orbiting spacecraft imposes many design challenges in the area of spacecraft thermal control and electrical power generation. The discovery mission MESSENGER (Mercury Surface, Space, Environment, Geochemistry, and Ranging), being designed and built by the Johns Hopkins University Applied Physics Laboratory (APL), will orbit and survey the planet Mercury for one year. In order to reduce cost and schedule risk while increasing the probability for mission success, the MESSENGER solar arrays will be constructed from conventional “off the shelf” materials and technologies
Keywords :
solar cell arrays; space vehicle power plants; testing; Johns Hopkins University; MESSENGER mission; Mercury Surface Space Environment Geochemistry and Ranging; Mercury orbiter spacecraft; cost reduction; dual sided array; electrical power generation; high intensity solar illumination testing; high temperature test programme; infrared testing; risk scheduling; solar panel development; solar panel testing; spacecraft thermal control; Costs; Mercury (planets); Physics; Planetary orbits; Planets; Prototypes; Solar power generation; Space missions; Space vehicles; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference and Exhibit, 2000. (IECEC) 35th Intersociety
Conference_Location :
Las Vegas, NV
Print_ISBN :
1-56347-375-5
Type :
conf
DOI :
10.1109/IECEC.2000.870725
Filename :
870725
Link To Document :
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