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