DocumentCode
1933940
Title
Low-mass high-performance deployable optical baffle for CubeSats
Author
Greenbaum, A. ; Knapp, Matthias ; Schaalman, G. ; Henderson, Tim ; Seager, Sara
Author_Institution
Charles Stark Draper Lab., Cambridge, MA, USA
fYear
2013
fDate
2-9 March 2013
Firstpage
1
Lastpage
12
Abstract
An optical moon baffle for stray light attenuation was developed for use on ExoplanetSat, a 3U CubeSat being developed jointly by MIT and Draper Laboratory which aims to detect transiting exoplanets via precision photometry. This paper will discuss the optical and mechanical design of the baffle, as well as the optical performance as demonstrated through the test of a prototype. The baffle collapses to fit into a small volume around ExoplanetSat´s lens and deploys on orbit to a full length of 12 cm. The baffle is capable of attenuating moonlight by a factor of 105 at a lunar exclusion angle of 30 degrees.
Keywords
Moon; artificial satellites; astronomical photometry; lenses; optical design techniques; optical testing; stray light; 3U CubeSat; CubeSats; ExoplanetSat lens; deployable optical moon baffle; lunar exclusion angle; mechanical design; moonlight attenuation; optical design; precision photometry; stray light attenuation; transiting exoplanet detection; Blades; Detectors; Electron tubes; Lenses; Moon; Optical attenuators; Stray light;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2013 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4673-1812-9
Type
conf
DOI
10.1109/AERO.2013.6496886
Filename
6496886
Link To Document