Fabry-Perot Based Ranging Interferometer Receiver for High Spectral Resolution Lidar

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$599,982.00
Award Year:
2009
Program:
SBIR
Phase:
Phase II
Contract:
NNX09CB25C
Agency Tracking Number:
074916
Solicitation Year:
2007
Solicitation Topic Code:
S1.01
Solicitation Number:
n/a
Small Business Information
Michigan Aerospace Corporation
1777 Highland Drive, Suite B, Ann Arbor, MI, 48108-2285
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
969868298
Principal Investigator:
David Johnson
Principal Investigator
(734) 975-8777
djohnson@michaero.com
Business Contact:
Pete Tchoryk
Chief Executive Officer
(734) 975-8777
jdodds@michiganaerospace.com
Research Institution:
n/a
Abstract
Michigan Aerospace Corporation (MAC) is pleased to present the following Phase II proposal for a Fabry-Perot Based Interferometer Receiver for the High Spectral Resolution Lidar (HSRL) System. Under the Phase I work, MAC successfully developed instrument models and created a conceptual design for an aircraft-qualified receiver that can be used with the current HSRL collection optics. This design is optimized to spectrally separate the aerosol and molecular backscatter for the calculation of the aerosol-to-total-scattering ratio and aerosol extinction coefficient. Additionally, wind and temperature data products can be produced with this system. The proposed Phase II efforts are directed at designing and building a bench-top HSRL 532nm receiver that is capable of taking accurate measurements of aerosol scattering ratio, extinction coefficients, molecular temperature and line-of-sight (LOS) velocity. This demonstration unit will verify a new adaptive interferometer measurement technique, called the Programmable Edge Technique (PET), which makes use of a Digital Micro-mirror Device (DMD) in conjunction with a Fabry-Perot interferometer and two photo-multiplier tubes (PMT). The completed bench-top receiver design will serve as the baseline for future aircraft mounted implementations.

* information listed above is at the time of submission.

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