DocumentCode
3203932
Title
Demonstration of the exoplanet detection process using four-beam nulling interferometry
Author
Martin, Stefan R. ; Booth, Andrew J. ; Loya, Frank
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
fYear
2009
fDate
7-14 March 2009
Firstpage
1
Lastpage
9
Abstract
The Planet Detection Testbed has been developed to simulate and test the detection process for an infrared nulling interferometer observing an earthlike planet orbiting a nearby star within about 15 pc of the solar system. The testbed combines eight beams of infrared light, four from the star and four from the planet, simulating an dasiaX-arraypsila telescope spacecraft formation. The detection process involves stable nulling of the starlight, rotation of the spacecraft formation, averaging over a few hours and testing of the signal against predicted exoplanet signatures. The testbed simulates all parts of the detection process except operation in broadband light, which is a planned upgrade for the future. This paper describes the latest results and plans for exoplanet signal simulation, deep starlight nulling and planet detection at star to planet contrast ratios of one million to one. These results are planned to demonstrate the feasibility of exoplanet detection using nulling interferometry at near-flightlike contrast ratios.
Keywords
aerospace instrumentation; astronomical instruments; extrasolar planets; interferometers; X-array telescope spacecraft formation; deep starlight nulling; exoplanet detection; exoplanet signal simulation; four beam nulling interferometry; infrared nulling interferometer; planet detection testbed; spacecraft formation rotation; Extrasolar planet; Infrared detectors; Laboratories; Optical control; Optical interferometry; Optical noise; Propulsion; Space technology; Space vehicles; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace conference, 2009 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
978-1-4244-2621-8
Electronic_ISBN
978-1-4244-2622-5
Type
conf
DOI
10.1109/AERO.2009.4839467
Filename
4839467
Link To Document