DocumentCode
3364786
Title
Spacecraft lighting systems
Author
Wheelwright, Charles D. ; Toole, Jennifer R.
Author_Institution
Lockheed Eng. & Sci. Co., Houston, TX, USA
fYear
1992
fDate
4-9 Oct 1992
Firstpage
1840
Abstract
A general description of the internal and external lighting systems is presented. The most appropriate light source for illumination of the interior of spacecraft is the fluorescent lamp. The primary approach and design criteria followed in the development and implementation of a luminaire are discussed, and an overview of the primary systems is given. In particular, the general illumination within the working and living areas should provide a medium level intensity of white light and utilize supplemental task lighting where functionally required. The luminaire should cover the entire work area with a uniform diffuse intensity. On most spacecraft, a variety of lighting systems are utilized to provide artificial illumination of the exterior visual scene during night side operations. These luminaires provide lighting for the following: extravehicular activity, acquisition tracking, rendezvous, berthing and docking operations
Keywords
fluorescent lamps; lamp accessories; lighting; space vehicles; berthing; design criteria; development; diffuse intensity; docking; extravehicular activity; fluorescent lamp; illumination; lamp accessories; lighting systems; luminaire; spacecraft; white light; Aerospace engineering; Displays; Floods; Fluorescent lamps; Hardware; LED lamps; Lighting control; Plasma chemistry; Space missions; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Industry Applications Society Annual Meeting, 1992., Conference Record of the 1992 IEEE
Conference_Location
Houston, TX
Print_ISBN
0-7803-0635-X
Type
conf
DOI
10.1109/IAS.1992.244541
Filename
244541
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