Millikelvin temperature control system for the ExoplanetSat Imager

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Earth, Atmospheric, and Planetary Sciences, 2012.

Bibliographic Details
Main Author: Li, Luyao
Other Authors: Sara Seager.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2013
Subjects:
Online Access:http://hdl.handle.net/1721.1/77789
_version_ 1811086157634600960
author Li, Luyao
author2 Sara Seager.
author_facet Sara Seager.
Li, Luyao
author_sort Li, Luyao
collection MIT
description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Earth, Atmospheric, and Planetary Sciences, 2012.
first_indexed 2024-09-23T13:21:43Z
format Thesis
id mit-1721.1/77789
institution Massachusetts Institute of Technology
language eng
last_indexed 2024-09-23T13:21:43Z
publishDate 2013
publisher Massachusetts Institute of Technology
record_format dspace
spelling mit-1721.1/777892019-04-12T21:41:28Z Millikelvin temperature control system for the ExoplanetSat Imager Li, Luyao Sara Seager. Massachusetts Institute of Technology. Dept. of Earth, Atmospheric, and Planetary Sciences. Massachusetts Institute of Technology. Dept. of Earth, Atmospheric, and Planetary Sciences. Earth, Atmospheric, and Planetary Sciences. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Earth, Atmospheric, and Planetary Sciences, 2012. Cataloged from PDF version of thesis. Includes bibliographical references (p. 50). ExoplanetSat is the prototype of a CubeSat-based space telescope for the discovery of transiting exoplanets around the nearest and brightest Sun-like stars. It is capable of monitoring a single target star from low Earth orbit, going through an orbit day-night cycle. In order to limit the noise induced by variable temperature, the temperature of the imaging device needs to be controlled within a steady level over the approximately 30 minutes of orbit night when the telescope is actively observing. In this thesis I present the design of a cold-biased system that controls the temperature of the irnager through passive cooling and active heating. The temperature is controlled by the system being heated to a slightly higher temperature than it's environment. The active control over the heater maintains the system at the target temperature within the 30 millikelvin range, with the best performance of 5 millikelvin control. The temperature control system can be used at various phases of ExoplanetSat development, including laboratory simulation of the temperature control of the ExoplanetSat imager during orbit night, characterizing the temperature response of any potential imager, and part of the design can be applied to the flight model of the prototype of ExoplanetSat for irnager temperature control. by Luyao Li. S.M. 2013-03-13T15:47:11Z 2013-03-13T15:47:11Z 2012 2012 Thesis http://hdl.handle.net/1721.1/77789 828099592 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 viii, 53 p. application/pdf Massachusetts Institute of Technology
spellingShingle Earth, Atmospheric, and Planetary Sciences.
Li, Luyao
Millikelvin temperature control system for the ExoplanetSat Imager
title Millikelvin temperature control system for the ExoplanetSat Imager
title_full Millikelvin temperature control system for the ExoplanetSat Imager
title_fullStr Millikelvin temperature control system for the ExoplanetSat Imager
title_full_unstemmed Millikelvin temperature control system for the ExoplanetSat Imager
title_short Millikelvin temperature control system for the ExoplanetSat Imager
title_sort millikelvin temperature control system for the exoplanetsat imager
topic Earth, Atmospheric, and Planetary Sciences.
url http://hdl.handle.net/1721.1/77789
work_keys_str_mv AT liluyao millikelvintemperaturecontrolsystemfortheexoplanetsatimager