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One-Dimensional Tunable Photonic-Crystal IR Filter

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNL07AA07C
Agency Tracking Number: 053484
Amount: $599,930.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: S6.01
Solicitation Number: N/A
Timeline
Solicitation Year: 2005
Award Year: 2007
Award Start Date (Proposal Award Date): 2006-12-01
Award End Date (Contract End Date): 2008-11-30
Small Business Information
2572 White Road
Irvine, CA 92614-6236
United States
DUNS: 188465819
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Vladimir Markov
 Principal Investigator
 (949) 553-0688
 vmarkov@metrolaserinc.com
Business Contact
 Christina Arnold
Title: Director of Administration
Phone: (949) 553-0688
Email: carnold@metrolaserinc.com
Research Institution
N/A
Abstract

MetroLaser proposes to design and develop an innovative narrowband tunable IR filter based on the properties of a one-dimensional photonic crystal structure with a resonant cavity. Such structure would exhibit an ultra-narrow, high-throughput band in the middle of a wide, low-transmission stop-band. During Phase I, through an extensive and detailed analysis, we performed a feasibility study to establish the operational characteristics and performance of the proposed tunable filter. Following this, we assembled and tested a breadboard and demonstrated filter tunability over 4 cm 1 with bandpass close to 0.25 cm-1, rejection level better than 23 dB, and acceptance angle of about 1 degree at 10.6 microns. The acquired data demonstrated our optimal approach for designing and constructing an ultra-narrow tunable optical bandpass filter. During Phase II, we will design, build, deliver to NASA, and perform field testing of a compact and robust prototype module of a 1" diameter narrowband filter with a tunability range of 10 cm-1, a bandpass range of 0.1 cm-1, background rejection of 30 dB, and transmittance better than 50%. A rugged and monolithic filter design will allow this instrument to be incorporated in air- or space-based platforms providing stable performance in harsh operating environments.

* Information listed above is at the time of submission. *

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