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Vacuum-Compatible Wideband White Light and Laser Combiner Source SystemFor the Space Interferometry Mission (SIM) Spectrum Calibration Development Unit (SCDU) testbed, wideband white light is used to simulate starlight. The white light source mount requires extremely stable pointing accuracy (<3.2 microradians). To meet this and other needs, the laser light from a single-mode fiber was combined, through a beam splitter window with special coating from broadband wavelengths, with light from multimode fiber. Both lights were coupled to a photonic crystal fiber (PCF). In many optical systems, simulating a point star with broadband spectrum with stability of microradians for white light interferometry is a challenge. In this case, the cameras use the white light interference to balance two optical paths, and to maintain close tracking. In order to coarse align the optical paths, a laser light is sent into the system to allow tracking of fringes because a narrow band laser has a great range of interference. The design requirements forced the innovators to use a new type of optical fiber, and to take a large amount of care in aligning the input sources. The testbed required better than 1% throughput, or enough output power on the lowest spectrum to be detectable by the CCD camera (6 nW at camera). The system needed to be vacuum-compatible and to have the capability for combining a visible laser light at any time for calibration purposes. The red laser is a commercially produced 635-nm laser 5-mW diode, and the white light source is a commercially produced tungsten halogen lamp that gives a broad spectrum of about 525 to 800 nm full width at half maximum (FWHM), with about 1.4 mW of power at 630 nm. A custom-made beam splitter window with special coating for broadband wavelengths is used with the white light input via a 50-mm multi-mode fiber. The large mode area PCF is an LMA-8 made by Crystal Fibre (core diameter of 8.5 mm, mode field diameter of 6 mm, and numerical aperture at 625 nm of 0.083). Any science interferometer that needs a tracking laser fringe to assist in alignment can use this system.
Document ID
20100001356
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Azizi, Alineza
(California Inst. of Tech. Pasadena, CA, United States)
Ryan, Daniel J.
(California Inst. of Tech. Pasadena, CA, United States)
Tang, Hong
(California Inst. of Tech. Pasadena, CA, United States)
Demers, Richard T.
(California Inst. of Tech. Pasadena, CA, United States)
Kadogawa, Hiroshi
(California Inst. of Tech. Pasadena, CA, United States)
An, Xin
(California Inst. of Tech. Pasadena, CA, United States)
Sun, George Y.
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2010
Publication Information
Publication: NASA Tech Briefs, January 2010
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NPO-46165
Distribution Limits
Public
Copyright
Public Use Permitted.
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