Prototype solar panel development and testing for a mercury orbiter spacecraft

被引：0

作者：

Ercol, CJ ^{[1
]}

Jenkins, JE ^{[1
]}

Dakermanji, G ^{[1
]}

Santo, AG ^{[1
]}

Mason, LS ^{[1
]}

机构：

[1] Johns Hopkins Univ, Appl Phys Lab, Laurel, MD 20723 USA

来源：

35TH INTERSOCIETY ENERGY CONVERSION ENGINEERING CONFERENCE & EXHIBIT (IECEC), VOLS 1 AND 2, TECHNICAL PAPERS | 2000年

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

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.

引用

页码：449 / 459

页数：11

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