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Long-duration Operation of 2-micron Coherent Doppler Lidar in SpaceThe reliability and lifetime of laser remote sensing systems that can operate autonomously over a sufficiently long period are mainly constrained by the laser diode arrays (LDAs) used for pumping their laser transmitters. The lifetime of a 2-micron coherent lidar operating in space is particularly of concern in lieu of required pump pulse duration of Thulium and Holmium solid state lasers (approx. 1msec) that are considerably longer than those of more widely used 1-micron lasers (< 0.2 msec). A factor of 5 to 10 times longer pulse duration can easily translate to over an order of magnitude shorter lifetime for a typical commercially available high-power 2-D array. Therefore, it is imperative to address the lifetime and reliability of LDAs for pumping 2-micron lasers by exploring all the potential options that significantly prolong their life meeting the required operational lifetime of space-based coherent Doppler lidars. The leading causes of sudden failure and premature degradation of LDAs are intrinsic semiconductor defects, optical facet breakdown resulting from excessive localized heating, and thermo-mechanical stresses due to the extreme thermal cycling of the laser active regions1-2. Long pulse operation grossly amplifies the impact of these failure/degradation causes, particularly the thermo-mechanical stresses due to pulse-to-pulse thermal cycling. Therefore, several experimental setups have been developed to investigate each of the failure mechanisms and causes of premature degradation in order to evaluate various package designs, define the best operating parameters, and to guide the technology advancement, leading to highly reliable and very long lifetime LDAs5. Several areas of improvement in the packaging and fabrication process of laser diodes have already been identified and efforts towards implementing these improvements are well underway. These efforts include the use of advanced high thermal conductivity materials for packaging of laser diode arrays and new fabrication techniques for mechanically attaching laser diode bars and submounts. But even using the existing LDAs, it may be possible to increase the lifetime by careful selection of the package type, number of bars per package and their pitch, operational temperature, and operating parameters such repetition rate, pulsewidth, and applied current. Obviously, the LDA specification and operational parameters will involve a system level trade analysis to ensure that the lidar instrument meets its performance objectives. One goal of this work is to enable such trade analysis by evaluating LDAs from different suppliers in different package types and quantifying their performance as a function of their operational parameters.
Document ID
20050238995
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Amzajerdian, Farzin
(NASA Langley Research Center Hampton, VA, United States)
Meadows, Byron L.
(NASA Langley Research Center Hampton, VA, United States)
Barnes, Bruce W.
(NASA Langley Research Center Hampton, VA, United States)
Baker, Nathaniel R.
(Lockheed Martin Engineering and Sciences Co. Hampton, VA, United States)
Baggot, Rene P.
(Science and Technology Corp. Hampton, VA, United States)
Kavaya, Michael J.
(NASA Langley Research Center Hampton, VA, United States)
Singh, Upendra N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2005
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Meeting Information
Meeting: 13th Coherent Laser Radar Conference
Location: Kamakura
Country: Japan
Start Date: October 16, 2005
End Date: October 21, 2005
Funding Number(s)
OTHER: 23-612-30-04-2L
Distribution Limits
Public
Copyright
Public Use Permitted.
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